Text

Reactor Containment Bldg Structural Integrity Test.
	ML19308D686
Person / Time
Site:	Crystal River
Issue date:	12/07/1976
From:	; GILBERT/COMMONWEALTH, INC. (FORMERLY GILBERT ASSOCIAT
To:	;
References
	GAI-1930, NUDOCS 8003120810
	Download: ML19308D686 (225)
	v • d • e

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CRYSTAL RIVER UNIT -

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NUCLEAR GENERATING PLANT REACTOR CONTAINMENT BUILDING STRUCTURAL INTEGRITY TEST

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PREPARED FOR: I FLORIDA - l i POWER ,

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DECEMBER 7,1976. GAI REPORT NO. 1930 CRYSTAL RIVER UNIT THREE NUCI. EAR GENERATING PLANT REACTOR CONTAINMENT BUILDING w

STRUCTURAL INTEGRITY TEST .

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FLORIDA POWER CORPORATION l

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l Gilbert Associates, Inc.

. P. O. Box 1498 Reading, Pennsylvania Geert/Commessene

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1 TABLE OF~ CONTENTS Section Title Pg 1

1.0 PURPOSE 1 l 2.0 SYNOPSIS 2 3.0 THE CONTAINMENT STRUCTURE 3 3.1 STRUCTURE DESCRIPTION 3 3.2 MATERIALS 4 3.2.1 Liner 4 3.2.2 Mild Steel Reinforc e nt 4 3.2.3 Concrete 5 3.2.4 Tendons 5 3.3 DESIGN 5 -

4.0 CONSTRUCTION METHODS 6 5.0 CONTAINMENT DOME REPAIR 7 6.0 TEST REQUIREMENTS 8 6.1 PRELIMINARY SAFETY ANALYSIS REPORT 8 6.2 FINAL SAFETY ANALYSIS REPORT 3 6.3 REACTOR BUILDING DOME DELAMINATION 8 6.4 REGULATORY REQUIREMENTS 8 7.0 TEST PROCEDURES 9 7.1 GENERAL DESCRIPTION 9 7.2 PREPARATION 10 8.0 INSTRUMENTATION 12

. 8.1 GENERAL DESCRIPTION 12 1 8.2 CONCRETE CRACK MEASUREMENTS 12 9.0 AS BUILT CONDITIONS 14 10.0 CALCULATED RESPONSE 16 I 10.1 GENERAL DESCRIPTION 16 10.2 DISPLACEMENTS 17 10.3 CONCRETE CRACK PATTERNS 18 11.0 EVALUATION OF DATA 21 11.1 DISPLACE!ENT AND STRAIN DATA 21 11.2 CONTAINMENT WALL DISPLACEMENTS 21 11.%.1 Vertical Displacements 21 11.2.2 Radial Displacements 21 Emet /Cammenesso i

m TABLE OF CONTENTS (Cont'd)

Section Title Pm 11.3 CONTAINMENT WALL STRAINS 22 11.3.1 Hoop Strains 23 11.3.2 Meridional Strains -

23 11.3.3 Liner Strains 23 11.4 DOME DISPLACEMENTS AND STRAINS 24 11.4.1 vertical Displacements 24 11.4.2 Dome Strains 24 11.5 EQUIP!CNT HATCH DISPLACEMENTS AND STRAINS 25 11.6 PENETRATION STRAINS 26 11.7 TENDON ANCHORAGES 26 11.8 CRACK PATTERNS 27 12.0 STRUCTURAL INTEGRITY TEST CONCLUSIONS 33 l

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s. , 1.0 PURPOSE This report presents a detailed description of the Structural Integrity Test (SIT) performed on the Crystal River Unit 3 Nuclear

-Generating Plant (CR3) reactor containment building during October and November 1976. During the SIT the reactor containment building was subjected to a maximum internal pressure of 63.3 psig. Figure 8 of Enclosure 1 presents dates, times and pressures for the SIT.

Conclusions related to the SIT are based on the observations and measurements made during the test and documented in this report.

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d m 2.0 SYNOPSIS Measurements and observations recorded during the SIT have been evaluated and compared with predictions of the expected structural behavior during the test. The data confirmed the expected behavior.

It is concluded that the CR3 reactor containment building, including the repaired dome, satisfies the requirements of the design criteria.

Test instrumentation performe( sasonably well and most of the recorded data are considered .s be valid. The few minor "

discrepancies in the data are noted and discussed in Section 11.0 of this report. The number of discrepancies was small compared to the amount of the data recorded during the test.

There was no evidence of structural instability during the test.

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Whitewashed areas and other areas which were inspected for cracks confirmed the predictions that minimal cracking would occur in the cylinder portion of the containment and that dome surface crack j patterns would be regular and uniform during the test. Strains and displacements were generally less than the theoretical and limit values. indicating that the analysis of the test condition was l conservative.

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m, 3.0' THE CONTAINMENT STRUCTURE 3.1 STRUCTURE DESCRIPTION The centainment structure is a post-tensioned concrete structure with cylindrical valls, a flat foundation mat and a shallow dome. The l cylindrical walls are prestressed in the vertical and hoop directions.

The dome is prestressed using a three-way post-tensioning system. In ;

addition to the prestress, mild steel reinforcing was placed in the cylinder and dome. )

i The inside surface of the building is lined with a carbon steel liner to ensure leak tightness. The liner shell. thickness is for the most l l

part 3/8 inch. The base liner is 1/4 inch thick. The liner in

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transition between the base liner and cylinder wall is 3/4 inch thick.

The foundation mat slab is reinforced with conventional mild steel reinforcing. The mat bears on competent material and is 12.5 feet j thick with a concrete slab 2 feet thick above the bottom liner plate.

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The cylinder has an inside diameter of 130 feet, a thickness of )

3 feet - 6 inches and a height of 157 feet from the top of the foundation slab to the spring line. The dome has a major radius of 110 feet, a transition radius of 20 feet - 6 inches and a thickness of 3 feet.

Two large openings are provided for access into the containment structure: one is a 22 foot - 4 inch inside diameter opening for the equipment access hatch; the other, a 10 foot inside diameter opening

'l for the personnel lock. Penetrations for main steam, feedwater, purge !

r air, other mechanical process piping and electrical cables are also

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w provi,ded in the cylinder wall. Drawings and a description of the containment structure are provided in the CR3 Final Safety Analysis Report (FSAR) and " Reactor Building Dome Delamination" report.

3.2 MATERIALS 3.2.1 Liner The basic liner plate conforms to ASTM A283-67, Grade C. Thickened portions of the liner at the crane girder and reinforcing around

. penetrations conform to ASME-ASTM SA516 Grade 60 or 70. ;

l Non-accessible liner seams are covered with A36 steel test channels to I

permit leak testing. Penetration sleeves through the containment )

barrier consist of material conforming to ASME-ASTM SA-333, Grade 1 and SA-300.

3.2.2 Mild Steel Reinforcement Mild steel reinforcement in the cylinder, dome, and reinforcement in j the mat conforms to ASTM A-615-68, Grade 40 and Grade 60. The reinforcing steel in the cylinder and dome provides capacity for bending and shear. The mat reinforcing steel provides capacity in tension, bending and shear.

No. 14 and 18 bars were spliced with Cadwelds capable of developing the ultimate strength of the bars. Bars of size number 11 or smaller were lap spliced, except for some of the reinforcement in the ring girder and repaired dome which were Cadwelded.

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3.2.3 Concrete The concrete mix used in the cylinder, dome and mat was designed to develop a minimum of 5000 psi compressive strength in 28 days. The in place strength of the dome concrete, based on the tests of concrete cores, is in excass of 6000 psi. Admixtures were used for air entrainment and water reduction.

3.2.4 Tendons The prestressing used for the reactor containment building is the BBRV system utilizing a maximum of 163, 7 mm diameter wires. These wires conform to ASTM A-421-65 Type BA with a guaranteed ultimate tensile l strength of 240,000 psi and use the BBRV button head system for end I

anchorages. Tendons are encased in galvanized steel conduits.

Tendons and included anchorages are coated with a temporary corrosion inhibitor for protection prior to bulk filling of the conduits.

3.3 DESIGN The methods and assumptions used for the design of the structure are described in the FSAR and the " Reactor Building Dome Delamination" report.

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, -4.0 CONSTRUCTION METHODS The containment liner for the cylinder and dome was erected ,

independently of placement of the concrete shell. Survey techniques were used to ascertain actual liner dimensions after construction.

Mild steel reinforcement for the cylinder is located on both faces with tendon conduits in between. Outside face concrete forms were tied to the liner on approximately 6 foot centers.

Dome tendon conduits (5" diameter Schedule 40 pipe) were pre-bent and ,

spliced as required to span frem one anchorage asse cly to the other

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for each tendon location. Dcme concrete was not placed until tendon

, conduits, trumpets, anchar plates and reinforcing bars were installed.

Tendons were stressed after the cylindrical wall and dome concrete has been placed and cured. Vertical tendons were stressed first. The stressing operation started at four positions along the circumference of the cylinder. The sequence of stressing vertical tendons was approxicately symmetrical with respect to the cylindrical wall circumference.. After completion of the vertical tendons, the hoop tendons were stressed in a sequence so as to minimize stress concentration in the shell. Then the dome tendons were stressed. For a description of the dome tendon stressing sequence see the " Reactor Building Dome Delamination" report.

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~'s- 5.0- CoffrAINMENT DOME REPAIR A complete history and documentation of the CR3 dome repair are presented in.the " Reactor. Building Dome Delamination" report. This document has been f11ed with the Nuclear Regulatory Commission (NRC).

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4 3 6.0 -TEST REQUIREMENTS 6.1 PRELIMINARY SAFETY ANALYSIS REPORT The CR3 Preliminary Safety Analysis Report (PSAR), Section 5.6 and Appendix SF, Reactor Building Instrumentation, provided background information on initial commitments to the NRC on the subject of instrumentation to be used and measurements to be made during the SIT.

2 6.2 FINAL SAFETY ANALYSIS REPORT Appendix SA of the CR3 FSAR provides a description of commitments for the SIT.

6.3 REACTOR BUILDING DOME DELAMINATION In order to ascertain that the repaired CR3 dome would function as intended, additional instrumentation was provided in excess of that defined in the FSAR. The additional instrumentation is described,in the " Reactor Building Dome Delamination" report.

6.4 REGULATORY REQUIREMENTS Prior to performing the SIT a comparison was made between the test requirements given in Appendix SA of the FSAR and those required by Regulatory Guide 1.18, " Structural Acceptance Test for Concrete Primary Reactor Containment." The differences between these two documents were found to be minor and the intent of Regulatory Guide 1.18 had been met.

Appendix J of the " Reactor Building Dome Delamination" report contains the correspondence between the NRC and Florida Power Corporation (FPC) concerning instrumentation of the dome for the SIT.

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., 7.0 TEST PROCEDURES 7.1 GENERAL DESCRIPTION The SIT procedure was developed such that the response of the reactor containment building would be measured as it was subjected to internal pressures from 0 psig to 63.3 psig and ba;k to O psig. The maximum test pressure, 63.3 psig, was 15 percent in excess of the design pressure, 55 psig, derived from the postulated maximum loss of coolant accident.

Pressurizaticn and depressurizatica were secomplished in stages to '

permit readings and measurements at the following pneumatic pressure levels: O psig, 12 psig, 35 psig, 45 psig, 55 psig, 63.3 psig, 55 psig, 45 psig, 35 psig, 12 psig and 0 psig. The 12 psig level readings were added during the test, at the request of Mr. W. Swan, NRC, I&E Division. When a data acquisition pressure level was reached, the pressure was held for one hour prior to acquiring data to permit the structure to adjust to the applied pressure.

During the pressurizacion phase and after the hold period was maintained at a data acquisition pressure level, the following measurements were recorded:

a. Cylinder and dome displacements,

b. Strain measurements of reinforcing bars and the liner.

c. Crack patterns and crack widch for whitewash areas.

d. General inspection of accessible exterior portions of the structure for cracking and possible interferences.

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'. During the depressurization phase only items a and b above were recorded. At the final zero pressure level all data was recorded.

1 A description 'o f the instrumentation used to measure the structural ;

response and the measurements and observations made during the SIT are included in Enclosure 1.

l Measurements and observations at each pressure level were comparad with predicted results and evaluated prior to pressurizing or l l

depressurizing to the next level.

.l Predicted displacements and strains are described in Section 10.0.

l The evaluation of test results is included as Section 11.0 of this i report.

7.2 PREPARATION )

A detailed test procecure was written prior to beginning the test. A 1

checklist of items which were signed off before pressurization began included the following:

a. Instruments necessary for mea' ;urements and equipment necessary for pressurization of the reacte containment building was available.

b. Auxiliary equipment necessary for taking measurements was available.

c. Prerequisite testing had been accomplished.

d. Possible interferences had been investigated.

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. e. Interior temperature of the reactor containment building had been stabilized.

f. Accessible exterior surfaces of the reactor containment building, tendon anchorage inspection areas and crack pattern areas had been inspected for cracks.

g. Exclusion areas had been established.

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8.0 INSTRUMENTATION 8.1 GENERAL DESCRIPTION Measurement and observation of the behavior of the reactor containment building ~during the test were accomplished using the following:

a. Displacement measurements Linear Potentiometers (LP).

b. Strain measurements

1. Linear strain gages.

2. Rosette strain gages.

3. A11 Tech concrete strain gages.

c. Concrete crack measurements

Optical comparators.

d. Miscellaneous

1. Electronic readout instruments for LP's and strain gages.

2. Thermocouples.

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The location and identification of the instrumentation used for each measurement is presented in Enclosure 1. j i

Installation of the instruments and the data acquisition system are also discussed in Enclosure 1.

8.2 CONCRETE CRACK MEASUREMENTS The accessible exterior surfaces of the reactor containment building were visually inspected for cracks and crack patterns before and during the test. Observed cracks' were charted; with the size of any i

cracks equal or exceeding .01 inches in width noted. '

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Approximately 1600 square feet of the exterior surface of the reactor containment building was whitewashed for measurement of spacing and width of cracks to confirm that the magnitude of local strains was not excessive. Whitewash areas were as fcilows:

a. An area of the structure approximately 6 feet wide extending 'from dome apex, across the top of the ring girder and down its side to a point 6 feet below it.

b. An area 6 feet by 6 feet on the cylinder at elevation 174'-0". .

c. An area 6 feet by 10 feet at the base of the cylinder.

d. An area of approximately 28 feet by 32 feet at one upper quadrant of the equipment access opening.

A one foot by one foot grid system was laid out on each whitewashed area. Platforms were provided for access and protective covers shielded the areas from adverse weather. Cracks were plotted for each pressure level (except at the 12 psig level-) when pressurizing and at 0 psig after completion of the pressure test.

The crack pattern charts are presented in Appendix D of Enclosure 1 to this report.

The general condition of a group of selected tendon anchorages was reported in the same manner as the crack patterns. The anchors inspected are listed on page 17 of Enclosure 1.

The reports at each pressure level are included in Appendix D of Enclosure 1.

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< 9.0 AS BUILT CONDITIONS A survey of the "as built" conditions of the reactor containment building was performed. This included a survey of the liner radius at several elevations as shown on Figure 9.1.

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ELEVATION R-l R2 R-3 R4 R-5 R6 R-7 R-6 R-9 R \O R-ll RA2 R-83 R-14 R 85 R-lO 24 5. #5~ ~ ~ G4.as4 G4.615 G4.77i G4333 GIsW G4.sai di.isii si.898 Gs o5s si.id's

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's 10.0 CALCULATED RESPONSE ,

10.1 GENERAL DESCRIPTION The reactor containment building was analyzed prior to the SIT for the 63.3 psig internal pressure load case.

The analyses took into account the actual strength of the concrete based on test cylinder results. The concrete modulus of elasticity (E) used was:

6 E = 4.0 x 10 Ksi Instantaneous Loads 0

E = 2.7 x 10 Kai Present Prestress Losses The value of Poisson's ratio (u) used was:

p = .17 The following properties were assumed for the liner:

E = 30 x 10 0 ,

u = 0.27 Two separate analyses were performed to obtain theoretical (predicted) values for the various test parameters. The general structure was modeled for the KALNINS STATIC computer program. This program was used for the analysis and the design cf the reactor containment building and was considered to be accurate for predictions of the overall behavior of the structure.

A second analysis was performed using a finite element

program to provide a more accurate prediction of test parameters around thickened _ local portions of the shell which could not be modeled using KALNINS STATIC computer program. These portions included the Geert /r-16

j N, buttresses, equipment access hatch and personnel access hatch. The model included the entire cylindrical portion of the shell from the top of the mat to the spring line.

10.2 DISPIACEMENTS Predicted and limiting displacements for each radial and vertical measurement point are given in Table 10.1. Pressure versus displacement plots for de data acquired during the SIT are presented in Appendix B of Enclosure 1. The predicted displacement at 63.3 is indicated by a circle, obtained from the analyses described in Sectien 10.1. The line labeled " LIMIT" includes an increase over the theoretical value to account for the precision of instruments, accuracy of readings, accuracy of loads and analytical techniques, and construction variables. Variables concerning instrumentation and measurements are discussed in the text of Enclosure 1.

The " LIMIT" at 63.3 psig was calculated by increasing the

" theoretical displacement" by'25 percent, plus 0.005 inches which was the full rangc' accuracy of the instruments used. These values were ." rounded off" to the nearest 0.005 inches. l For example, if the " theoretical displacement" at 63.3 psig were

.200 inches, the " LIMIT" includes 0.005 inches for the measurement accuracy and 25 percent of 0.20 inches, or 0.05 inches, for the analytical modeling:

.200 + .05 + .005 = .255 inches i

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s, 10.3 CONCRETE CRACK PATTERNS Stress cracking in the cylinder from the applied pressure loading was not anticipated dua to the residual compressive stress remaining in the shell at 63.3 psig. It was expected that existing shrinkage cracks would enlarge slightly in width and propagate in length during reactor containment building pressurization.

In the dome cap where prestressing was minimal', a pattern of regularly spaced cracks was anticipated. The width of the cracks was expecte6 to be small due to the presence of non-prestressed reinforcing steel.

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TABLE 10.1 Displacement Acceptance Criteria Theoretical Limiting Gage Displacement Displacement Tolerance ID Measurement (inches) (inches) (inches) 1, 2, 3 Radial 0.010 0.020 0.010 4,5,6 Radial 0.090 0.115 '.025 i

7,8,9 Radial 0.205 0.260 0.055 10, 11, 12 Radial 0.200 0.255 0.055 13, 14, 15 Radial 0.205 0.260 0.055

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16, 17, 18 Radial 0.160 0.205 0.045 19, 20, 21 Radial 0.060 0.080 0.020 22, 23, 24 Radial -0.025' -0.040 -0.015 25, 26, 27 Radial -0.055 -0.070 0.015 28,,29, 30 Vertical 0.215 0.275 0.060 34 Vertical 0.905 1.135 0.230 35 Radial 0.10 0.130 0.030 35 Vertical 0.10 0.130 0.030 36 Radial 0.08 0.105 0.025 36 Vertical 0.10 0.130 0.030 37 Radial 0.12 0.155 0.035 37 Vertical 0.10 0.130 0.030 38 Radial 0.115 0.150 0.035 38 Vertical 0.10 0.130 0.030 39 Radial 0.115 0.150 0.035 39 Vertical 0.10 0.130 0.030 9

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TABLE 10.1 Displacement Acceptance Criteria (Cont'd)

. Theoretical Limiting Gage Displacement Displeement Tolerance ID Measuremenc (inches) (inches) (inches) 40 Radial 0.11 0.140 0.030 40 Vertical 0.10 0.130 0.030 41 Radial 0.11 0.140 0.030 41 Vertical

0.10 0.130 0.030 42 Radial 0.11 0.140 0.030 42 Vertical 0.10 0.130 0.030 43 Radial 0.090 0.120 0.030 43 Vertica'l 0.105 0.135 0.030 44 Radial 0.090 '

O.120 0.030 44 Vertical 0.105 0.135 0.030 45 Radial 0.095 0.125 0.030 45 Vertical 0.110 0.140 0.030 46 Ladial 0.100 0.130 0.030 46 Vertical 0.11 0.140 0.030 47 Radial 0.105 0.133 0.030 47 Vertical 0.115 0.150 0.035 48 Radial 0.110 0.140 0.030 48 Vertical 0.120 0.155 0.035 128, 129, 130 Radial 0.040 0.055 0.015 128, 129, 130 Vertical 0.365 0.460 0.095 164, 165, 166 Vertical 0.900 1.130 0.230 4

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. 11.0 EVALUATION OF DATA 11.1 DISPLACEMENT AND STRALN DATA Enclosure 1 contains computer printouts, sketches and data collected during the SIT. It also contains an explanation of the types of instruments used and their locations.

11.2 CONTAINMENT WALL DISPLACEMENTS 11.2.1 Vertical Displacements Vertical displacements for the containment wall were measured at 3 azimuths, 90 degrees, 200 degrees and 334 degrees, at the ring girder, elevation 267'-6", (Enclosure 1, Appendix B, Figure 21 and Table 23). These displacements were regular with the difference between the readings at 63.3 psig being .021 inches. The displacements w' era less than the predicted displacement which was

.215 inches with a limiting value of .275 inches. The actual values at 63.3 psig were .171 inches (at 90 degrees); .180 inches (at '

200 degrees); and .192 inches (at 334 degrees). The residual deforr.ations were small and when converted to equivalent stress i values, the maximum was less than 50 psi.

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11.2.2 Radial Displacements l

Radial displacementa for the containment wall were measured at 3 azimuths, 90 degrees, 200 degrees, and 334 degrees at a eievations

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(see Enclosure 1, Appendix B, Figure 21 and Table 24) . Figures 9, 10, and 11 of Enclosure 1 show plots of these displacements at various pressure levels and Appendix B,shows plots of individual gage points. These displacements are regular and in good agreement with each other and with the predicted values. Table 11.1 indicates the values of the displacement'at 63.3 psig.

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. The major variation appears to be due to a greater resistance to rotation of the ring girder than was predicted.' Although the structure at 270'-8" was predicted to move outward due to rotation, (the top of the cylinder moves in) it actually moved slightly inward. l l

This would indicate that the ring girder is stiffer in relation to l I

the dome than assumed in making the calculations. No adverse affect I on either the dome, ring girder or cylind,er can be attributed to ;

this.

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Radial displacements for each elevation were generally less than ' l limiting values. Although some of the smaller displacements exceeded l the limiting value, these were small in the absolute sense and no adverse effects can attributed te them.

11.3 CONTAINMENT WALL STRAINS The strains for t nta ament wall were measured with gages attached to the liner (Enclosure 1, Aprendix A, Figure 18 and Table

12) and to reinforcing bars in the crea of the dome cylinder transition (Enclosure 1, Appendix A, Figure 13 and Tables 6 through 11). The strains around openings and penetrations will be discussed in later sections.

On Page 19 of Enclosure 1, under TEST RESULTS, some of the specific problems resulting from the long delay between gage placement and actual testing are discusset.. Some of the gages appear to have excessive " shake down" values, that is gage adjustment during the initial loading from 0 to 63.3 psig. Although these readings were not excessive in most cases, the value for strain change for the "second loading", that is from 63.3 to O psig is considered more accurate and is used in most casas for comparisons..

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. 11.3.1 Hoop Strains Table 11.2 indicates the actual and predicted values of hoop strains in microinches per inch. When two gages exist for a point, the result closest to the predicted value is reported in these tables.

Results indicate low strains which are reasonably consistent with the i

predicted values. The strains at the upper elevations reflect lower values which are consistent (th deflection readings.

11.3.2 Meridional Strains Tabla 11.3 presents values of meridional strains. As with the hoop ~

strains, the meridional strains were small., In this case the actual f

l rotational behavior of the ring girder is strongly registered in very l large relative differences between predicted and measured values ia 1

the upper elevations. The negative strains which would have resulted l

l from the inward rotation of the top of the ring girder are p'ositive l due to the relative outward rotation. No detrimental effects are

- attributed to this difference in ==pected and actual bahavior.

11.3.3 Liner Strains The strains for the liner in the hoop and meridional directions are reported as part of Section 11.3.1 and 11.3.2. The gages used to measure these strains were Rosette type and are described on page 23 of Enclosure 1 The values of recorded strain are found in Table 12

_of Enclosure 1, Appendix A. Figure 20 of Appendix A illustrates how l

the Rosette rr.adings are reduced to maximum, minimum an- shear l l

[ strains. Thase values are given in tabular form by gage number under l

LINER GAGES in Appendix A. Also included is the stresa computed from I

these values. All the values computed are small with the exception I

i Geert/Casumenesse 23

.. .. a..-

of gage 71 and this gages behavior would indicate at least one of its elements is malfunctioning. There is no indication of detrimental strains in the liner.

11.4 DOME DISPLACEMENTS AND STRAINS 11.4.1 Vertical Displacements Vertical displacements for the dome were measured at the apex and at horizontal distances from the apex of approximately 29' (the fourth spray ring), 49' (elevation 270'-8") and 56' (elevation 267'-6") .

The results of the measurements are given in Enclosure 1, Appendix B, Table 23. The predf.cted values which include the wall deformation are included in Table 10.1. Data for individual gage locations are plotted in Enclosure 1, Appendix B. The displacement data are uniform, close to redicted values and within the " LIMIT" shown in each figure. The residual displacements at the end of the SIT were less than 15% of the maximum reading which is within the expected performance for this type of structure.

11.4.2 Dome Strains Additional gages were added to permit more complete evaluation of strains during the SIT. Enclosure 1 describes these gages and Figure: 14 and 19 of Appendix A indicate plan and through thickness locations. Tables A and B of Appendix A provide a listing of the gage numbers at each location. Tables 13, 14 and 15 indicate the meridional strains at each location and Tables 16,17 and 18 the hoop strains.

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I Because of the different type gages used; SR4 strain gages attachef to reinforcing, AIL TECH concrete strain gages and Rosette gages attached to the liner, variations in the readings were expected.

Table 11.4 compares the strains at the four through' thickness locations with predicted values. The strains are low and although variable indicate a reasonable correlation with predicted values. No detrimental effects are indicated by any of the results.

T.n addition to measurements in the membrane direction, a series of radial bars were instrumented in order to confirm that little or no radial tension or' deformation was taking place during the SIT.

Tables 19 through 21 present radial strain results. The strains are too small to allow valid numerical comparisons. For example, a strain of 50 microinches per inch would correspond to less than 1500 pri stress in the radial reinforcing.

11.5 EQUIPMENT HATCH DISPLACEMENTS AND STRAINS The displacements recorded at the equipment hatch are given in .

Enclosure 1, Appendix B, Tables 25 and 26, and are plotted on individual graphs in that Appendix. The locations of the measurement points are shs n in Figuro 23. The vertical

- displacements are all less ttun predicted. They tend to be more erratic than the radial gage readings during pressurization and depressurizatien although this may be due to the very small vaJues being recorded. The radial displacements tend to follow tht predicted slopes more closely with gages 38, 39, and 40 indicating slightly greater displacements than the limiting values set at 63.3 psig. However, the excess is slight and the instrument recovery was good with no ind.ication of detrimental effects.

l i Geert/Cummamamm 25 -

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,, Strain results for the equipment hatch are presented in Enclosure 1, Appendix A, Tables 1 and 2. The meridional strains like the vertical displacements tend to be erratic. However, all values are quite small (maximum compression of 115 microinches per inch and a maximum tension of 100 microinches per inch). This would reflect a maximum steel stress of 3,400 psi.

11.6 PENETRATION STRAINS The Rosette type strain gages were located on the metal liner at the main steam line penetration, the feedwater line penetration and at '!

one spare penetration. Figures 15, 16, 17, and 18 indicate the location of the penetrations and the gages. Enclosure 1, Appendix A, Figure 20 illustrates how the gage readings were reduced to maximum, minimum, and shear strain values. This appendix also includes the l strain values and their equivalent stresses for each of the penetrations. Several of the gages appear to have malfunctioning I 1

elements and did not record data which corresponded to the physical response of the structure. However, these gages (96, 98, 99, 100, 101, 102, 104, 105. 71, and 163) do not negate the results.

11.7 TENDON ANCHORAGES l No special instrumentation or surveillance of tendon anchorages was conducted during the test. Experience indicates that load cells installed under the button heads and strain gages placed on the bearing plates would not aid in the evaluation of the containment structure. This is due to the fact that the strains recorded would i-l Geert/Casuunmuunk 26

.- - _ _ , . . - - - .- - - ~-.:w A.~

be caused by the increase in tendon force resulting from the pressure m

loading. This increase amounts to only a small percentage of the total force in the tendon.

Visual inspection of the concrete at specified anchorage zones was accomplished prior to the start of the test, at each pressurization level and at the final zero. The results are reported in Appendix D on Data Sheet 6, TENDON ANCHORAGE OBSERVATION. No unusual cracking, bearing plate displacement or other unexpected occurrences were

, observed during the test. -

11.8 CRACK PATTERNS The results of the observation for cracking are shown in the crack pattern figures of Appendix D and confirm the original predictions.

The absence of stress cracking provides direct evidence that residual compression stress existed in this cylindrical shell at the peak pressure of 63.3 psig. The uniform nature of the cracks in the new dome cap at 63.3 psig,' as well as the subsequent closing of these cracks with the removal of the pressure load indicate that the dome was responding elastica 11y.

Existing shrinkage cracks were observed to enlarge slightly in width and length during the test. Some new hairline cracks did appear which were not initially observed. In all cases, crack patterns were random except in the dome cap. Crack widths were less than

.01 inches at peak pressure in all areas except in the dome cap.

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_s In addition to the inspections in white wash areas, other areas in reactor containment building were inspected for cracks during the

. test. This inspection included accessible ateas of the containment such as the dome and the intersection of the buttress and cylinder.

4 O

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3, TABLE 11.1 Radial Displacement @ Peak Pressure (63.3 psig)

(inches)

Elevation Predicted Value Observed Values Average (feet) Theoretical Limiting 90 200 334 Value 98 .01 .02 .031 .038 .036 .035*

108 .09 .115 .124 .106 .098 .109 140 .205 .260 .175 .244 .211 .210 172 .200 .255 .171 .205 .195 .190 I 204 .205 .260 .087 .138 .127 .117 236 .160 .205 .062 .114 .076 .084 246 .060 .080 .042 .026 .039 .005 253~ .025 .040 .053 .011 .007 .016 l l

267-6 .055 .070 .114 .071 .081 .088* '

l 270-8 . 040 .055 .120 .004 .007 .043*

l l

4

Value exceeds or varies in sign from predicted.

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e TABLE 11.2 Containment Wall Hoop Strains (63.3 psig)

'(p inches / inch)

Elevation Predicted ActualDifgerence (feet) Val e 90 200 333 Average 172 167 200

163 181 204 88 220 249

235 244 152 146 153 123 141 249 181 69 148 151 123

~

254 229

79 51 65 200 -

223 89 89 87 88 266 405 46 38 125 77 268 391 102 l'12 102 106 s

Malfunctioning Gage.

30

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1 w TABLE 11.3 Containment Wall Meridional Strains (63.3 psig)

(p inches / inch)

Predicted Elevation Value 90 ActualDifference 200 333 Average 172 252 143 73 50 88 204 258 ~59 109 167 109 244 106

84 120 102 249' 28 15 48 103 55 255 -62 156 166 179 167 260 -79 118 192 148 153 266 -104

359 307 333 268 94 320

269 295

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TABLE 11.4 Dome Strains (63.3 psig)

( 11 inches / inch)

Predicted ActuagDifferenge Location Value 75 165 255 345 Average 15' from apex 1H 324 -

321 210 -

265 M 313 - 205 182 -

199 2H 324 -

194 237 -

215 M 317 -

236 294 -

265 3H 324 - * * -

M 320 -

137 -

137 -

4H 324 - 240 280 -

260 M 343 -

253 -

253 30' from apex 1H 492 431 - -

420 426 M 354 533 - -

617 575 2H 461 483 - -

606 545 M 348 265 - -

364 315 3H 431 * - - *

M 343 * - - *

4H 231 227 - -

170 199 M 298 217 - -

193 205 45' from

, apex 1H 497 108 346 242 104 200 M 220 200 144 255 414 253 2H 465 185 297 215 453 287 M 199 78 136 236 158 152 3H 433

103

83 93 M 178 * * * *

4H 241 163 163 230 243 200 M 48 57 280 40 167 131

Malfunctioning Gage. *

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_. a.w . w w w.La:w wo>a u 12.0 STRUCTURAL INTEGRITY TEST CONCLUSIONS m .

The summary of Enclosure 1, pr.sa 31 provides an excellent statement

of the engineering conclusions of the test. These are as follows

a. The overall response of the structure was well substantiated.

l The diaplacements observed were uniform between identical points ,

on various azimuths. The displacements observed were within predicted values and were typical of displacements measured on other similar structures. The recovery observed was within

.i limits one would normally expect for a structure of this type. . !

l

, b. Cracking observed on the done was slightly greater than would l normally be expected in a prestressed dome but substantially less and of a smaller magnitude than could be expected in a reinforced done. The crack widths (under 0.01 inches) were such that they did not substantially increase steel stresses in the dome. The fact that at atmospheric pressure the cracks closed indicated that the structure was still within'the elastic 2

range.

c. The strains recorded for the reinforcing steel were well within the elastic range of this material. This indicates that the structure cauld undergo more deformation before any significant signs of distress would appear.

It is concluded that the structural response of the Crystal River Unit 3 Nuclear Generating Plant reactor containment building was ,

satisfactory during the SIT and demonstrates its capability to withstand postulated pressure loads. I GeertICommesmuse 33 s

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STRUCTURAL RESPONSE OF SECONDARY CONTAINMENT W

i DURING STRUCTURAL INTEGRITY TEST AT I.

CRYSTAL RIVER PLANT - UNIT 3

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FLORIDA POWER CORPORATION WJE No. 71465 n

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November 23, 1976 i

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- . . . . , . -- ---- ~ ~-x<w+a TABLE OF CONTENTS Title M ENCLOSURE 1 WISS, JANNEY, ELSTNER AND ASSOCIATES REPORT SCOPE 1 OBJECTIVES 2 DESCRIPTION OF THE SECONDARY CONTAINMENT 2 TEST PROGRAM 3 FIGURE 1 - REACTOR BUILDING - CROSS SECTION 4 STRAIN CAGE INSTRUMENTATION 6 FIGURE 2 - REINFORCING BAR STRAIN GAGE ASSEMBLY - DU1MY 7 DISPLACEMENT INSTRUMENTATION 9 FIGURE 3 - TYPICAL INSTALLATION FOR CONCRETE GAGES AT DOME 10 FIGURE 4 - INVAR WIRE EXIENSOMETER 12 TEMPERATURE INSTRUMENTATION 13 DATAACQUISITIONSISTEM 13 CRACK INSPECTION 14 FIGURE 5 - DATA ACQUISITION SYSTEM 15 FIGURE 6 = DATA ACQUISITION ROOM 16 STRUCTURAL INTEGRITY TEST 17 FIGURE 7a - TYPICAL PLATFORM - DOME TEEON INSPECTION 18 FIGURE 7b - DOME CRACK INSPECTION AREA 1ROTECTIVE COVER 18 TEST RESULTS 19 Stresses In Reinforcing Steel 19 FIGURE 8 - TIME-PRESSURE CURVE 20 Stresses In Liner Plate 23 Stresses In Concrete 24 i

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TABLE OF CONTENTS (Cont'd)

Title M

RADIAL DISPT.ACEMENT OF CYLINDER WALL 24 FIGURE 9 - RADIAL DISPLACEMENIS-CYLINDER WALL - AZIMUTH 90 25 FIGURE 10 - RADIAL DISPLACEMENTS-CYLINDER WALL - AZIMUTH 200 26 FIGURE 11 - RADIAL DISPLACEMENTS-CYLINDER WALL - AZIMUTH 333-55 27 CYLINDER GROVIH AND DOME DISPLACEMENTS 28 EQUIPMENT HATCH DISPLACEMENIS, 28 TEMPERATURE RESULTS 29 CRACK _ PATTERNS 29 DEVELOPMENT OF CRACKS DURING TEST 30

SUMMARY

31 APPENDIX A -STRAIN DATA FIGURE 12 - EQUIPMENT ACCESS OPENING - STRAIN GAGE REINFORCING BAR LOCATION A -l FIGURE 13 - STRAIN GAGE GROUP LOCATIONS A-2 FIGURE 14 - TYPICAL SECTION AT INSTRUMENT LOCATION A-3 FIGURE 15 - ROSETTE GAGE LOCATION - INTERIOR FACE, MAIN STEAM PENETRATION A-4 FIGURE 16 - ROSETTE GAGE LOCATION - INTERIOR FACE, FEEDWATER PENETRATION A-5 FIGURE 17 - ROSETTE GAGE LOCATION - SPARE PENEIRATION, INIERIOR FACE A-6 FIGURE 18 - ROSEITE LOCATIONS ON WALL A-7 FIGURE 19 - CONCRETE GAGE LOCATIONS AT DOME A-8 TABLE A - DOME STRAIN INSTRUMENTATION A-9 TABLE B - INSTRUMENTED RADIAL ANCHOR LOCATIONS A-10 TABLE 1 - EQUIPMENT. HATCH MERIDIONAL STRAINS A-ll TABLE 2 - EQUIPMENT HATCH HOOP STRAINS A-12 ii 9% gg--

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.___ .._.m-- ..- _; e -. R ., w , . m m.444 e v w n TABLE OF CONTENTS -(Cont'd) ytp Page TABLE 3 - MAIN STEAM LINE PENETRATION STRAINS A-13 TABLE 4 - FEEDWATER LINE PENETRATION STRAINS A-14 TABLE 5 - SPARE PENEIRATION STRAINS A-15 TABLE 6 - CYLINDER WALL AND DOME JUNCTION MERIDIONAL STRAINS AZIMUTH 90 A-16 TABLE 7 - CYLINDER WALL AND DOME JUNCTION MERIDIONAL STRAINS AZIMUTH 200 A-17 TABLE 8 - CYLINDER WALL AND DOME JUNCTION MERIDIONAL STRAINS AZIMUTH 333-55 A-18 TABLE 9 - CYLINDER WALL AND DOME JUNCTION HOOP STRAINS AZIMUTH 90 A-19 TABLE 10 - CYLINDER WALL AND DOME JUNCTION HOOP STRAINS AZIMUTH 200 A-20 TABLE 11 - CYLINDER WALL AND DOME JUNCTION HOOP STRAINS AZIMUTH 333-55 A-21 TABLE 12 - WALL LINER STRAINS A-22 TABLE 13 - DOME MERIDIONAL STRAINS - RADIUS 45 FEET A-23 TABLE 14 - DOME MERIDIONAL STRAINS - RADIUS 30 FEET A-24 TABLE 15 - DOME MERIDIONAL STRAINS - RADIUS 15 FEET A-25 TABLE 16 - DOME HOOP STRAINS - RADIUS 45 FEET A-26 TABLE 17 - DOME HOOP STRAINS - RADIUS 30 FEET A-27 TABLE 18 - DOME HOOP STRAINS - RADIUS 15 FEET A-28 TABLE 19 - DOME RADIAL STRAINS - RADIUS 45 FEET A-29 TABLE 20 - DOME RADIAL STRAINS - RADIUS 30 FEET A-30 TABLE 21 - DOME RADIAL STRAINS - RADIUS 15 FEET A-31 TABLE 22 - DOME LINER STRAINS A-32 FIGURE 20 - ROSETTE DATA OUTPUI KEY A-33 111

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TABLE OF CONTENTS (Cont'd)

Title Pg MAIN STEAM LINE PENETRATION ROSETTE NUMBER 76 ' A-34 ROSETTE NUMBER 77 A-34 ROSETTE NUMBER 78 A-34

' ROSETTE NUMBER 79 A-35 ROSETTE NUMBER 80 A-35 ROSETTE NUMBER 81 A-35 ROSETTE NUMBER 82 A-36 ROSETTE NUMBER 83 A-36 ROSETTE NUMBER 84 A-36 ROSETTE NUMBER 85 A-37 ROSETTE NUMBER 86 A-37 ROSETTE NUMBER 87 A-37 ROSETTE NUMBER 88 A-38 ROSETTE NUMBER 89 A-38 FEEDWATER LINE PENEIRATION ROSETTE NUMBER 90 A-39 ROSETTE NUMBER 91 A-39 ROSETTE NUMBER 92 A-39 ROSETTE NUMBER 94 A-40 ROSETTE NUMBER 95 A-40 ROSETTE NUMBER 96 A-40 ROSETTE NUMBER 98 A-41 ROSETTE NUMBER 99 A-41 ROSETTE NUMBER 100 A-41 ROSETTE NUMBER 101 A-42

~ ROSETTE NUMBER 102 A-42 SPARE PENETRATION ROSETTE NUMBER 104 A-43 ROSETTE NUMBER 105 A-43

. ROSETTE NUMBER 108 A-43 ROSETTE NUMBER 109 A-44 ROSETTE NUMBER 110 A-44 ROSETTE NUMBER 111 A-44 ROSETTE NUMBER 112 A-45 ROSETIE NUMBER 113 A-45 ROSETTE NUMBER 114 A-45 ,

ROSETIE NUMBER 115 A-46 l ROSETTE NUMBER 116 A-46 j ROSETTE NUMBER 117 A-46 l

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TABLE OF CONTENTS (Cont'd) x Title Page LINER GAGES ROSETTE NUMBER 70- A-47 ROSETTE NUMBER 71 A-47 ROSETTE NUMBER 72 A-47

, ROSETTE NUMBER 73 A-48 ROSETTE NUMBER 74 A-48 ROSETTE NUMBER 75 A-48 ROSETTE NUMBER 134 A-49 ROSETTE NUMBER 142 A-49 ROSETIE NUMBER 138 A-49 ROSETIE NUMBER 146 A-50 ROSETTE NUMBER 151 A-50 ROSETTE NUMBER 155 A-50 .

ROSETTE NUMBER 159 A-51 ROSETIE NUMBER 163 A-51 APPENDIX B - DISPLACEMENTS FIGURE 21 - RADIAL DISPLACDIENTS - CYLINDER WALL B-1 FIGURE 22 - CYLINDER WALL DISPLACEME ITS B-2 FIGURE 23 - PLAN VIEW - INSTRUMENTATION FOR EQUIPMENT ACCESS B-3 TABLE 23 - VERTICAL DISPLACEMENTS B-4 TABLE 24 - CYLINDER WALL RADIAL DISPLACEMENTS B-5 TABLE 25 - EQUIPMENT HATCH VERTICAL DISPLACEMENTS B-6 TABLE 26 - EQUIPMENT HATCH RADIAL DISPLACEMENTS B-7 RADIAL DISPLACEMENT - LOCATION 1 - AZIMUTH 90 ELEV. 98'-0" B-8 RADIAL DISPLACEMENT - LOCATION 2 - AZIMUTH 200 ELEV. 98'-0" B-9 RADIAL DISPLACEMENT - LOCATION 3 - AZIMUTH 330-55 ELEV. 98'-0" B-10 RADIAL DISPLACEMENT - LCCATION 4 - AZIMUTH 90 ELEV. 108'-0" B-ll RADIAL DISPLACEMENT - LOCATION 5- - AZIMUTH 200 ELEV. 108'-0" B-12 RADIAL DISPLACEMENT - LOCATION 6 - AZIMUTH 333-55 ELEV. 108'-0" B-13 RADIAL DISPLACEMENT - LOCATION 7 - AZIMUTH 90 ELEV. 140'-0" B-14 RADIAL DISPLACEMENT - LOCATION 8 - AZIMUTH 200 ELEV. 140'-0" B-15 RADIAL DISPLACEMENT - LOCATION 9 - AZIMUTH 333-55 ELEV. 140'-0" B-16 RADIAL DISPLACEMENT - LOCATION 10 - AZIMUTH 90 ELEV. 172'-0" B-17 RADIAL DISPLACEMENT ~- LOCATION 11 - AZIMUTH 200 ELEV. 172'-0" B-18 RADIAL DISPLACEMENT - LOCATION 12 - AZIMUTH 333-55 ELEV. 1.72'-0" B-19 RADIAL DISPLACDfENT - LOCATION 13 - AZIMUTH 90 ELEV. 204 '-0" B-20 RADIAL DISPLACEMENT - LOCATION 14 - AZIMUTH 200 ELEV. 204'-0" B-21 RADIAL DISPLACEMENT - LOCATION 15 - AZIMUTH 333-55 ELEV. 204'-0" B-22 V

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TABLE OF CONTENTS (Cont'd)

'N

Title Pm RADIAL DISPLACEMENT -

LOCATION 16 - AZIMUTH 90 ELEV. 236'-0" B-23 RADIAL DISPLACEMENT -

LOCATION 17 - AZIMUTH 200 ELEV. 236'-0" B-24 RADIAL DISPLACEMENT -

' LOCATION 18 - AZIMUTH 333-55 ELEV. 236'-0" B-25 RADIAL DISPLACEMENT -

LOCATION 19 - AZIMUTH 90 ELEV. 246'-0" B-26 RADIAL DISPLACEMENT -

LOCATION 20 - AZIMUTH 200 ELEV. 246'-0" B-27 RADIAL DISPLACEMENT -

LOCATION 21 - AZIMUTH 333-55 ELEV. 246 '-0" B-28 RADIAL DISPLACEMENT - LOCATION 22 - AZIMUTH 90 ELEV. 253'-0" B-29 RADIAL DISPLACEMENT -

LOCATION 23 - AZIMUTH 200 ELEV. 253'-0" B-30 RADIAL DISPLACEMENT -

LOCATION 24 - AZIMUTH 333-55 ELEV. 253 '-0" B-31 RADIAL DISPLACEMENT -

LOCATION 25 - AZIMUTH 90 ELEV. 267'-0" B-32 RADIAL DISPLACEMENT -

LOCATION 26 - AZIMUTH 200 ELEY. 267'-0" B-33 RADIAL DISPLACEMENT -

LOCATION 27 - AZIMUTH 333-55 ELEV. 267'-0" B-34 VERTICAL DISPLACEMENT - LOCATION 28 - AZIMUTH 90 ELEV. 270'-8" B-35 VERTICAL DISPLACEMENT - LOCATION 29 - AZIMUTH 200 ELEV. 270'-8" B-36 -

VERTICAL DISPLACEMENT - LOCATION 30 - AZIMUTH 330-55 ELEV. 270'-8" B-37 VERTICAL DISPLACEMENT - LOCA' ION 34 - DOME APEX B-38 EQUIPMENT HATCH RADIAL DISPLACEMENT - LOCATION 35 - AZIMUTH 160 ELEV. 132'-0" B-39 EQUIPMENT HATCH VERTICAL ~ DISPLACEMENT - LOCATION 35 - AZIMUTH 160 ELEV. 132'-0" B-40 EQUIPMENT HATCH RADIAL DISPLACEMENT - LOCATION 36 - AZIMUTH 150 ELEV. 120'-0" B-41 EQUIPMENT HATCH VERTICAL DISPLACEMENT - LOCATION 36 - AZIMUTH 150 ELEV. 120'-0" B-42 EQUIPMENT HATCH RADIAL DISPLACEMENT -

LOCATION 38 - AZIMUTH 126 ELEV. 132'-0" B-43 EQUIPMENT HATCH VERTICAL DISPLACEMENT - LOCATION 38 - AZIMUTH 126 ELEV. 132'-0" B-44 EQUIPMENT HATCH RADIAL DISPLACEMENT -

LOCATION 39 - AZIMUTH 131 I ELEV. 132'-0" B-45 EQUIPMENT HATCH VERTICAL DISPLACEMENT - LOCATION 39 - AZIMUTH 131 ELEV. 132'-0" B-46 EQUIPMENT HATCH RADIAL DISPLACEMENT - LOCATION 40 - AZIMUTH 134 ELEV. 132'-0" B-47 EQUIPMENT HATCH VERTICAL DISPLACEMENT - LOCAT'ON 40 - AZIMUTH 134 ELEV. 132'-0" B-48 EQUIPMENT HATCH RADIAL DISPLACEMENT -

LOCATION 41 - AZIMUTH 137 EQUIPMENT HATCH ELEV. 132'-0" B-49 VERTICAL DISPLACEMENT - LOCATION 41 - AZIMU'. 137 ELEV. 132'-0" B-50 EQUIPMENT HATCH RADIAL DISPLACEMENI -

LOCATION 42 - AZIMUTH 139 EQUIPMENT HATCH ELEV. 132'-0" B-51 VERTICAL DISPLACEMENT - LOCATION 42 - AZIMUTH 139 ELEV. 132'-0" B-52 EQUIPMENT HATCH RADIAL DISPLACEMENT - LOCATION 43 - AZIMUTH 150 ELEV. 144'-0" B-53 EQUIPMENT HATCH VERTICAL DISPLACEMENT - LOCATION 43 - AZIMUTH 150 ELEV. 144'-0" B-54 EQUIPMENT HATCH l RADIAL DISPIACEMENT -

LOCATION 44 - AZIMUTH 150 ELEV. 147'-0" B-55 vi

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-- 2 ~ c -mawasaw TABLE OF CONTENTS (Cont'd) 3 Title Page EQUIPMENT HATCH VERTICAL DISPLACEMENT -

LOCATION 44 - AZIMUTH 150 ELEV. 147'-0" B-56 EQUIPMENT HATCH RADIAL. DISPLACEMENT LOCATION 45 - AZIMUTH 150 ELEV. 151'-0" B-57 EQUIPMENT HATCH VERTICAL DISPLACEMENT -

LOCATION 45 - AZIMUTH 150 ELEV. 151 '-0" B-58 EQUIPMENI HATCH RADIAL DISPLACEMENT - LOCATION 46 - AZIMUTH 150. ELEV. 155'-0" B-59 EQUIPMENI HATCH VERTICAL DISPLACEMENT -

LOCATION 46 - AZIMUTH 150 ELEY. 155'-0" B-60 EQUIPMENT HATCH RADIAL DISPLAC MENT -

LOCATION 47. - AZIMUTH 150 ELEV. 159'-0" B-61 EQUTPMENT HATCH VERTICAL DISPLACEMENT -

LOCATION 47 - AZIMUTH 150 ELEV. 159'-0" .B-62 -

EQUIPMENT HATCH RADIAL DISPLACEMENT -

LOCATION 48 - AZIMUTH 150 ELEV. 163'-0" B-63 EQUIPMENT HATCH VERTICAL DISPLACEMENT -

LOCATION 48 - AZIMUTH 150 ELEV. 163'-0" B-64 RADIAL DISPLACEMENT -

LOCATION 128 - AZIMUTH 90 ELEV. 270'-8" B-65 VERTICAL DISPLACEMENT -

LOCATION 128 - AZIMUTH 90 ELEV. 267'-6" B-66 VERTICAL DISPLACEMENT -

LOCATION 129 - AZIMUTH 200 ELEV. 167'-6" 4 B-67 RADIAL DISPLACMENT -

LOCATION 129 - AZIMUTH 200 ELEV. 270'-8" B-68 RADIAL DISPLACEMENT -

LOCATION 130 - AZIMUTH 333-55 ELEV. 270'-0" B-69 ~

VERTICAL DISPLACEMENT -

LOCATION 130 - AZIMUTH 333-55 ELEV. 267'-6" B-70 VERTICAL DISPLACEMENI -

LOCATION 164 - AZIMUTH 90 ELEV. 4th Spray Ring B-71 VERTICAL DISPIACEMENT -

LOCATION 165 - AZIMUTH 200 ELEV. 4th Spray Ring B-72

. VERTICAL DISPLACEMENT . -

LOCATION 166 - AZIMUTH 333-55 ELEV. 4th Spray Ring B-73 APPENDIX C - TEMPERATURE DATA FIGURE 24 - AMBIENT TEMPERATURE - CYLINDER WALL C-1 TEMPERATURE READINGS C-2 to C-10

' APPENDIX D - CRACK INSPECTION AREA No.118 - BASE SLAB AND CYLINDER D-1 to D-4 AREA NO.119 - CYLINDER MID HEIGHT D-5 to D-8 AREA NO.120 - RING BEAM AND DOME D-9 to D-30

. AREA NO. 121 - EQUIPMENI HATCH D-31 to D-34 TENDON ANCIORAGE OBSERVATION D-35 to D-40 vii

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TABLE OF CONTENTS (Cont'd) s Title Page APPENDIX E -COMPUTER OUTPUT - SAMPLE EQUIPMENT HATCH MERIDIONAL STRAINS E-1 EQUIPMENT HATCH HOOP STRAINS E-2 PENETRATION STRAINS MAIN STEAM LINE E-3 PENETRATION STRAINS FEEDWATER LINE E-4 RADIAL DISPLACEMEhTS E-5 EQUIPMENI HATCH VERTICAL DISPLACEMENTS E-6 EQUIPMENT HATCH RADIAL DISPLACEMENTS E-7 I

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4 viii

)

1

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m .,

f STRUCTURAL RESPONSE OF SECONDARY CONTAISMENT W

[s,. DURING STRUCTURAL INTEGRITY TEST AT

, y CRYSTAL RIVER PLANT - UNIT 3 a-n n

g FOR E '

s FLORIDA POWER CORPORATION t'

n -

I November 23, 1976 a

k A

j SCOPE 8

i

, a The stmactural behavior study described hereunder was performed I during the structural integrity test of the secondary containment vessel, Unit No. 3, Crystal River, Florida. Wiss, Janney, Elstner and Associates were retained by Florida Power Corporation to install the !

l

( prescribed instrumentation, monitor the response of the instruments, j 1

conduct crack surveys prior to and during structural integrity testing, and to report on the results of this structural behavior study. !

'The location of test instrumentation was planned by Gilbert Associates, Incorporated. The work was performed in accordance with Gilbert Associates, Inc. Specifications No. SP5971 and No SP-6488.

All installation was performed or supervised by WJE personnel. That part of the work normal to their skills (routine installation of electrical lead wire, welding, etc.) was performed by site craf t

's labor.-

l

.- 1

.a. .-~-.. : . .. . -

~~ . -~~ n e-m N . OBJECTIVES l

The instrumentation was planned to serve two purposes. l gy First, the satisfactory response of the structure to specific test i

I, pressures; second, confirmation of the criteria assumed in the

(-

n structural design.

e Y-DESCRIPTION OF THE SECONDARY CONTAINMENT E

I s

t The reactor building is a reinforced concrete structure composed ,

e r of a cylindrical wall with a flat foundation mat and a shallow dome roof.

a 2 The sideaalls rise 157 ft from the top of the base mat-(Elev. 93'-0")

ik to the springline of the dome (Elev. 250'-0"). The sidewalls are 3 ft s

f a

6 in. thick and the dome is 3 ft 0 in. thick. The cylinder walls are j prestressed with a post-tensioning system in the vertical and horizontal directions.

4 Major discontinuities occur in the structure at the following locations:

A. At Azimuth 150', thickened boss area around equipment hatch opening, Centerline Elevatica 132 ft 0 in.

B. At Azimuth 323*, a thickened boss area around the personnel lock, Centerline Elevation 122 ft 7 in.

C. At electrical and pipe penetrations. These t

j areas are not thickened. ,

._ u. . .s -as- _. - . __m . :, su

?

1, '

The interior wall of the containment vessel is lined with a 3/8 in. thick steel plate, continuously velded to form an airtight NV seal.

1 -

s

s. The done roof is prestressed utilizing a three-way post-J n

a tensioning system. A major portion of the concrete above the top n

y, layer of prestressing tendons is essentially a non-prestressed y conventionally reinforced section. This section is connected to the s

{ ; estressed dome portion by a series of radial anchors. The radial I

a anchors are #6, Grade 60 reinforcing bars, hooked into the top portion of the concrete. The Reactor Building Cross Section is shown in A

l Fig. 1.

8 i

TEST PF0 GRAM i

Test instrument. tion was located to yield the following information:

1. Radial displacement of the wall from -

Elevation 98 ft 0 in. to Elevation 270 ft 0 in, on Azimuths 90*, 200* and 333" - 55' .

2. Vertical growth of the cylinder and dome displacements of the structure.

-3 . Radial and vertical displacements around the 1

equipment hatch.

4. Hoop and Meridional strains in the reinforcing steel around the equipment hatch.

_. l

-+ -- - ' " " ~ ' ' " -

k EL. 285'-4 W.'

TOP OF 0 N6

/ GIRDER EL.267-G 5 u

. G.,

u bo I.

k 'fo

$, SPRING LINE ,

EL. 250'-O" 4

\-

4 k k s O, t 9 .

=

0

.8 h

h e 1

=

65'-O8 R. _

=

3 1-Gu pgg3 8/e' LINER k r= n 4 W =-

3 m

o. z 3

O -

i. __

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/ .

y st.ss'-d i k

'r d U [i" e

R.EA,CTOR BUILDiMG -

CROSS SECTION FIGURE .1.

l .

5. Hoop and Meridional strains in the reinforcing Ny steel at the ring beam on Azimuchs 90*, 200*

i

!, and 333* - 55'.

J a

g 6. Liner strains on the cylinder wall at Elevations e

I' 172 ft and 204 ft at Azimuths 90*, 200* and E

, 333* .55'.

t

~

e r

7. Liner strains around the Main steam penetration, a

S Feedwater penetration and Spare penetration.

A s

o 8. Hoop and Meridional strains in reinforcing steel c

i a of the new dome concrc:e.

I l

9. Strains in the radial anchor bars co'nnecting in the new and old dome concrete.

10. Hoop and Meridional strains in the dome concrete below the prestressing tendons.

11. Hoop and Meridional strain on the liner plate of the dome.

12. ' Ambient temperatures at Elevations 267'-6",

194'-0" and 122'-0" on Azimuth 90* and at Elevations 267'-6", 172'-0", 122'-0" on Azimuth 200*.

\

1

__;> h .ed,5 w l - -mm . : -

c.- .M .. . / > - ' w.~ XM --

s .,

13. -Crack patterns at the following locations:

a) The discontinuity at the equipment yy ' hatch i

5.

b) On the cylinder wall near the base slab a

n on Azimuth 270* at Elevation 93'-0" e

Y, E c) On the cylinder wall, at Elevation 172'-0" I

s t on Azimuth 270*

e r

a d) On the ring beam and dome on Azimuth 200*

h j 6 ft below the ring beam and continuing to s

a the apex of the dome.

c i

a e) Both ends of the twenty-one surveillance

{

t endons .-

In addition to the instrumentation above, a continuous visual inspection of the entire structure was made to monitor major cracking which might occur.

All whitewashed areas were protected from the elements with Visqueen tents.

STRAIN GAGE INSTRUMENTATION Strain information was obtained by mounting electrical resistance strain gages directly to the main reinforcing or to sister bars which were subsequently installed at the proper locations. Electrical

. resistance strain gages mounted on reinforcing bars or sister bars were

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RiGio POLvVINYL. CHl ORIDE CONOutf DETAll. A.A j d F4' HEAVY WALL. CAPPE D AT .

DOTH ENDS IG GA W8RE 4 M58 48 REINF BR 6

REINFORCING BAR STRAIM GAGE ASSEMBLY- DUMMY i

' cevc co-cov seAi_ c., To vu.. -

1 E - .= I ew so$, _

. . .. . __ L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _

ky' A' A' ,Y W A' N r'WFA' A' AMMN2-N-AM1 1 \\ .

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3 CONDuCTUR- IG eAGE WIRE +4 W5'C'RElHR O.R (

Goo V NEEOMECHE COVEREO CABLE DLie FAST -120 12 S G 2 ELEMENT GAGES ON BAR BPV 150. APPLIED TO BAR.

THCH WATER FEIOQI~ LNG AHD L.ACQUER f, I

DETAIL A-A

, .s c

(

FIGURE 2 i-t u _ _ _ _ _ _ _ _ _ _ _ _ _ _.__ __ _ _ ___ _ _ __ _ .- __ _ _ . _ __

,i . - , _ . r- _ = - u. n ... - -~ : . --_was wm-4 Y

/

~.,

two-element (temperature-compensating) SR4, encapsulated gages.

The following types wer2 used

]f s

1. SR4-BLH Type FABT-28-12S6 s, -

2. SR4-MM Type EA-06-125-TA-120 J

a -

n n Sister bars were fabricated using 3 ft sections of #4 rein-e Y.

E f rei g bar. The strain gages were attached to the bar using BLH-EPY150 I

s epoxy. After the lead wires were attached, the installation received t

n -

I a layer of silicone lacquer and two overlays of epoxy. The entire a

g installation was then encased in rigid polyvinyl chloride conduit, which

/L s

was subsequently filled with wax. (Fig. 2) s

@ To verify the adequacy of each assembly, each instrumented bar 1

i was continuously submerged in water for a minimum of 48 hours5.555556e-4 days 0.0133 hours 7.936508e-5 weeks 1.8264e-5 months . After soaking the resistance to ground was checked. Any installation showing a resistance to ground of less than 1000 megohms was deemed to be defective and was not used in the structure. The sister bar assemblies discussed above were fabricated at the laboratories of WJE and chipped to the site for incorporation in the structure.

Installation of the fabricated units consisted of wiring the

" gaged" bar to the appropriate reinforcing bar in the structure. The lead wires were then run to the exterior wall where they were terminated in a junction box.

Strain gages were applied directly to the main reinforcing steel at Locations 35 through 69. (A sister bar was also used at each location.

The term sister bar and dummy bar are interchangeable terms). The field installation of these gages consisted of attaching the strain

us. w, . .. .~.ww -

. _:. w.w aw,a- mn x

gage =vich EPY 150, attaching the lead wires, coating the installation with silicone lacquer and finishing with two coats of epoxy.

[

s Strain gages attached to the steel liner were SR4 -Type FABR 8' 12S9 three-element rosettes. Liner gages were attached with EPY 150.

J g The gages were then waterproofed as described previously, n

y, Concrete strains in the lower portion of the dome were moni-E tored with concrete embedment gages. The gages used were Model CG129 3

s n manufactured by-AIL TECH, Inc. The gag's e were cast in 5 in. by 2 in. .

I

, waffers at the WJE labroatory. Because these gages were to be S installed prior to removal of the top concrete, it was deemed practical A

I to provide a package that needed only to be grouted in the proper O

{

t location. The gage system was sent to the field where it was installed I in a 6 in. core hole, which had been drilled at the proper locations.

(See Fig. 3). 1 l

1 DISPLACEMENT INSTRUMENTATION l

Radial displacements from Elevation 98 to 270'-8" and all vertical measurements (except equipment hatch verticals) were obtained using invar wire extensometers.

The invar wire extensometers were located entirely within the structure, and were connected to an external power supply and readout equipment by electrical leads which extended through penetrations in the cylinder wall.

Each installation consisted of a extensometer and a invar wire spanning the distance to be measured. One end (the " dead" end) was fixed to the steel liner, and the " live" and of the wire was attached i- . - - . _. - _-__

_ . - . -, ... -~. . - . . . ~ .- - -

w di MLTECH STRAIN GAGES CYLINDER t_S" Ole-9 .

A "g -

e IL TY PI CAL WAF:FE R.

INSTAL I ^TICM GAGES ISS ,137,141,14.5 3 15 03 154,158, IG2 NEW CON CRE i t=.

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CLD CONCRETEj i

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CYLINDER I

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TYPICAL INSTAL i ATION l FOR CONCRETE GAGE.S AT DOME I l

FIGURE 3 I

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ll

_, ,_ _ G '

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s, to a spring-loaded frame which was attached to rigid supports or interior walls in the direction of measurement. Deformations of the

)[ structure were measured with a linear potentiometer mounted in each frame. (The spring and potentiometer arrangement is shown in Fig. 4).

J The potentiometers are of the infinite resolution type with a total e

y, resistance of about 2000 ohms. A constant voltage of 1.5615 volts E

1 s

was applied to each potentiometer. At each measurement, voltage is t

g measured between the movable contact point and one end of the resistor.

r a The voltage changes are recorded on the external readout system.

k Radial measurements above Elevation 172'-0" were made by A

s g bringing the invar wire diagonally down from the point of measurement c

1 to a fixed point on the operating floor. Additional vertical t

I measurements were made at these same locations. The true radial movement was then calculated using the diagonal radial growth and the vertical movement at each location.

Prior to shipment to the field, all the frames were calibrated in our laboratory. In addition all instruments vare calibrated in placc. The field calibration provided verification that each unit was accurrate to + 0.005 inches.

Vertical measurements at the aquipment hatch were made using spring-loaded linear potentiometers. The potentiometers were mounted on a rigid frame in close proximity to the containment wall. The potentiometer plunger rested on clip angles velded to the containment liner. Field calibration of these units was performed as previously described.

^

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INVAR WIRE EXTENSOMETER FIGURE 4

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TEMPERATURE INSTRUMENTATION Temperatures of the containment wall were measured at six NV g -locations using Leeds and Northrup Company Type J, #14 AWG Iron-s Constantine wire. The temperatures were monitored using a Leeds J ~

$ and Northrup Speedomax Model J-6000 strip chart recorder.

o

. r.

E DATA ACQUISITION SYSTEM i

s t

g A computer based automatic data acquisition system was sat -

r a up to obtain and process all the strain and deformation measurements k

during the test. The test station was located just outside the A

s s personnel lock and all results were made available to GAI engineers c

1 present at the test site.

t I The data acquisition system consisted of a Vidar Autodata Eight data logger interfaced with a Hewlett-Packard HP 9830 desk computer.

The system is shown schematically in Fig. 5. The Vidar Autodata Eight is a microprocessor-controlled system used to read raw analog data from input transducers and transform it into digital form. The system included three Vidar Scanners equipped to handle up to 800 input channels. The Autodata Eight is connected to the HP 9830 computer via ElA Standard RS-232-C Serial interface. The HP 9830 is a stand-alone desk computer with 15808 bytes of Read / Write memory. The computer output is printed on a thermal printer at the rate of 250 lines per minute.

The. computer was set up to scan at the rate cf one channel per second.

The data was stored on a magnetic tape cassette for permanent record and.further processing.

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u., -,.w. : a.-- , - _ . ~ -a . . ~ _ . - , w w w w - +:-

N All data acquisition functions were initiated and controlled from the HP 9830 computer. The data was recorded for 489 input

' TpI channels. At any pressure level the operator was required only to key in th( current pressure and execute the start command. The J

a computer was programmed to initiate the scan and check each channel n

); for overload and store all the voltage readings along with pressure, fs time of scan on the tape cassette. After all the data was collected, n the program would compute the incremental strains or deformations for '

I each gage using the original "zero" pressure reading and the necessary S calibration factors. The results were printed in a page format and A

e were submitted to GAI engineers. The data acquisition system would 8

i read 489 channels, process the data and print it in proper format in a

f approximately 20 minutes. A sample output of the results is s*.mn in Appendix E.

The reliability and accuracy of the acquired data were checked, where applicable, using a resistor calibration box. The calibrator incorporates a precision resistor of known magnitude which, when switched into the system, produces a known voltage change. Any significant deviation from the theoretical voltage change would indicate a malfunction in the system.

The data acquisition system is shown in Fig. 6.

l CRACK INSPECTION ;

Prior to the structural integrity test, the entire structure was surveyed for cracks. The survey was made from scaffolding, roof tops 4

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ANALJOG TRANS DUCEER INPUT .

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HEWLETT-PACKARD 8

VIDAR r

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9850 AUTODATA <-

DESK COtAPUTER sism ER FACE T

mTreRanNG DVM wcweweesex -

-?

MISC. CONTROLS r

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DATA ACQUISITION SYS i t=M t f

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.3 DATA ACQUISITION ROOM FIGURE 6 i

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1 and accessible walkways. Crack vidths observed during the pressure tast were measured using a 6X comparator.

NV i Visual observations of the total exterion surface were made at k

designated pressures during the test (35, 45, 55, 63.3 psig).

J n The following tendon anchors were inspected for concrete crack n

k. development et the same pressure levels as above:

E I D 121 12V20 13H10

! D 140 23V15 13H19 y D 203 34V6 13H37

~

r a D 215 45V3 51H30

$ D 324 56V1 51H41 j

D 339 53H17 j 53H32 g 53H47 1

" 62Hil 64H21 1

Both shop and field buttenheaded ends were checked. The inspection of the tendon ends was made from sky climbers, skip box and platforms positioned at the proper locations.

Fig. 7A and B shows, respectively, a typical platform for dome tendon inspection and the doue with its protective cover over the crack inspection area.

STRUCTURAL IlrrEGRITY TEST The structural integrity test was performed prior to the integrated leak rate test. Complete sets of data, were made at five pressure increments during the loeding cycle and at four pressure increments during depressurization (i.e., 12, 35, 45, 55, 63.3 55, 45, 35,12 psig) and finally at return to atmospheric pressure. Detailed

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i

,- 3 crack inspections were made during pressurization at 35, 45, 25, 63.3 psig and at atmospheric pressure.

During pr'essurization and depressurization all data points were 39 i

[ read and printed out every 5 psi. The data was obtained "on the run" (pressurization was not stopped). These intermediate readings allowed

{n ,

S GAI engineers to monitor'the structural response throughout the test. l' Y,

E At those designated test points i.e., 35, 45 etc., pressurization (or !

I 1

s depressurization) was stopped and the structure was allowed to stabilize l y -1 r for one hout. Readings and crack inspections were not started until a

@ this one hour stabilization period had passed. (Additional readings

{f were obtained immediately upon reaching each plateau). All readings were reduced and submitted to Gilbert Associate engineers for their i

4 t review before proceeding to the next pressure level. Only those readings I

obtained at designated hold points have been incorporated in the tabulated data.

The structural integrity test started on October 31, 1976 at 1103 hours0.0128 days 0.306 hours 0.00182 weeks 4.196915e-4 months and officially ended on November 3, 1976 at 1208 hours0.014 days 0.336 hours 0.002 weeks 4.59644e-4 months . A

~

time-pressure curve is presented in Fig. 8.

TEST RESULTS Stresses In Reinforcing Steel Two-element strain gages were mounted directly on the main steel and on redundant sister bars at the same location. This procedure was used for all locations around the equipment hatch and ring girder

, (Gage Nos. 35 through 69). The gage locations are shown on Figs.12 and 13 in Appendix A. .

. i "RESSURE (PSI.G) ' j.

NOTE s

SIT DATA POINTS i

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es -

, s 1

55 -

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T

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TIME l-IRS 2400 2400 2400 2400 l OATS io-ai-ve l - -ve l i i ve l i i 7e 1 PRESSURE VERSUS TIME , STRUCTURAL INTEGRITY TEST FIGURE 8 i

r

. .~ ~ .a - - . wm-u w-- - -- - w, m s..

s Hoop and meridional steel strains in the repaired portion of the dome were monitored using two independent sister bars, at each yy. location, wired to the main steel. The typical gage locations are i

( shown in Fig. 14 Appendix A. Table A, Appendix A identifies the gages.

J' Strains in the radial anchors were measured using field I

y ' installed strain gages on each bar. Redundancy for each anchor was Y.

E obtained by instrumenting the next closest anchor, i.e., Location 1

{ L20N17 the parent bar, Gage No. 171 and Location L 21N18 is redundant.

n - l I The typical gage locations are shown in Fig. 14 of Appendix A. I a

@ Identification of the gage numbers is shown in Table A and B of j f[ Appendix A.

c A total of 220 gages were installed on reinforcing bars, a

t (This number represents 110 measuring points). The following gages I

exhibited excessive drif t and instability, and have been excluded I

from this report, i 41M* 49M 65M 5'9H l 42M 56M 65M* 61H 45M 57M 66M 62H 47M 58M 67H 63H 35H 59M 67H* 64H 36H 62M 69M 65H 38H 63M 69M* 68H 45H 64M 55H 69H

Redundant Gages 69H The exclusion of these gages in no way negates the results obtained from the remaining gages. Due to the redundancy of the gages, a complete response picture was obtained.

The total number of gages listed above exhibit a mortality rate in excess of what would normally be expected on an installation of this type. A number of circumstances are believed to be contributing factors

- - - ~ ~ . ~ >x a -

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N in this mort ality rate. The original SIT was ocheduled for mid April. At this time all gages already installed were terminated 4

vv with temporary wiring to the data acquisition center. In checking 3 -

k the sages at this time it was found that five years after the a

n original installation only. ten (10) were suspect. Approximately 4

f four days prior to the test date problems in the dome were E discovered. Between May and October major repairs were made to the h

t done. Although every possible precaution was taken to procee; I

a wiring, damage did occur, due to the extent of the repair. It is

$ the writer's opinion that the high loss of gages can be attributed to A

e moisture reaching the gages through breaks or Farns in the lead wire.

g It is also the writer's opinion that the losses which were observed a

f were well below those which could have been expected under these conditions. '

4

= Steel strains measured throughout the structure were low, 200 microinches or less. Nkximum strains observed in the repahad portion of the done was 794 tieroinches, vien the majority of strain 500 microinches or less.

At completion of the test a review was made of gages showing inconsistencies with other gages in certain groups. It was suspected l that Gages 131H, 152H, 157M, 157H, 149M and 149H had been wired wrong causing a sign reversal. This sign reversal has been corrected in this report.. It was also suspected that Gage 144M had been interchanged with Gage 143M'and that Gage 144R had been interchanged with Gage 143H*.

These gages have been interchanged for this report.

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- - a. n , .. _ a.. u. -

S Stresses In Liner Plate yv Strain ga'ges were located around the main steam penetration, i .

I, feedwater penetration and a spare Penetration. The location of

( these gages are shown in Figs.15,16 and 17 in Appendix A.

R g Additional gages were located on the cylinder wall at Azimuchs 90*,

E 200*, and 333' - 55' at Elevations 172 ft and 204 ft. Fig. 18 1

a g shows the location of these gages, e -

Liner strains were measured at locations corresponding to a

S measurements made on the main reinforcing steelin the dome. Typical locations A

e of these installations are shown in Fig. 14 of Appendix A. Table A 8

y of Appendix A, lists actual gage numbers and locations.

a e Where applicable, the strain data obtained from each element s

of the rosette have been reduced to determine the principal stresses 0

at each gage location. A Modulus of Elasticity of 29 x 10 was used in the calculations. Fig. 20 indicates the key to the direction of the major and minor prfncipal stresses and maximum and minimum shears as related to the vertical and horizontal direction of the rosette.

All these stresses are shown in Appendix A.

The maximum principal stresses found in the liner plate appear reasonable. In most cases, the orientation was found to be close to the hoop disection.

During the course of the test, single elements of rosettes 93, 97, 103, 106 and 107 exhibited unstable readings. These gages have therefore not been included in the rosette reduction program.

Rosette No. 92 exhibited a false reading at 55 psi on depressurization, subsequently, this reading has been eliminated from the program.

_n . , u, ; w . ,. w .a .

. n _ ,- m...

Stresses In concrete Hoop and meridional strains were monitored in that portion lpI of the original concrete not removed during the repair of the dome.

The locations correspond to measurements made on the main steel.

J a Fig.19 in Appendix A, show the location of these gages.

n y, Gages 133, 137M, 141M, 145M and 150M showed excessive drift fs and have not been included in the tabulated data. In general, jr the concrete strains were low, 137 microstrain being the maximum ,

, observed. Most of the concrete strains were less than 100 microstrain S at peak pressure.

A s

The data for these gages are presented in.Tcbles 14 through 19 in Appendix A.

{

RADIAL DISPLACEMENT OF CYLINDER WALL Radial displacements of the cylinder wall were measured with invar wire extensometers at Azimuths 9P*, 200* nud 335*. At each Azimuth, instruments were at elevations shown on Fig. 21 of Appendix B.

Table 24 of Appendix B provides the deflections observed during the 4

test. The individual deflection plots are also presented in Appendix B.

Radial displacements of the cylinder wall have been plotted for each Azimuth. Figs. 9, 10 and 11 show the radial displacement of each wall

-for the pressure cycle only.

,g, ,.-e.e sw g"~a * - * ' - = - - - - * - - -- -

r**

. . _ , . - . . = . .

t 275-B - -

2E7-B - -

y 2E3-B --

245-B - - k 235-B - -

2BM-B - - -

! ? PStG -- . i b!, PSIG 45 PSIG 55 PSIG 172-B - - 63 PSIG %

i l

l l

145-B - -

IBB-B - -

1 BB-B - - 3 4

93-B BR5E ELRE ELEY. I

-B.2 -B.! B.B B.! B.2 ;

l RHDIRL D15PLHCEMENT5 DF CYLINDER WRLL(IN.) l RZIMUTH 90 l

FIGURE 9

. . . . ~ . ..a...... .x= -. .

~. .._ ..~ _~_ an -a.

~

t 275-B - -

2B7-B - -

p 2E3-B - -

24E B - - d 238-B - - '

V 2BM-B - - ~

12 PSIG %

35 PSIG 45 PSIG 55 PSIG 172-B - -

63 PSIG i

l 195 -

IBB-B - -

sB-B - -

S3-B DREE ELRB ELEY.

-B.2 -B.I B.B -

B.! B.2 RBDIRL DISPLREMENT5 OF CYLlHDER WRLL(IN.)

RZIMUTH 200 1

l FIGURE 10 l

2-~~.-

t 27B-8 --

257 -

y 2E3 --

\

2ME-B - -

23E-B - -

2B4-B - -

12 PSIG C 35 PSIG 45 PSIG 55 PSIG 172 -

63 PSIG%

N x N

N t

14B-B - - I l ' l IBB-B - -

BB-B - -

53-5 BREE ELRE ELEY.

l l

-B.2 -B.! B.B B.! 5.2 RRDIRL D15PLIKEMDlT5 DF CYLINDER WRI.L(IN.)

RZlMUTH 333-EE FIGURE 11

a.-.. .

w .~

_. ~ _ - ~ . .~ u_

CYLINDER GROWTH AND DOME DISPLACEMENTS TV The vertical growth of the cylinder was measured relative to the i

k base slab on three Azimuth, i.e., 90*, 200* and 333*. The displace-J a ment of the apex of the dome was measured relative to the operating n

), floor. Fig. 22 of Appendix B shows the location of vertical measurements, f

s Vertical growth of the dome, observed, was between 80% and 83%

d _of the predicted displacements at all locations. The instantaneous

, recovery, measured after a one hour hold at zero pressure, was 85%

2 or better for all points. Additional recovery could be expected if A

8 readings could have been obtained at a later time.

1 a The test data has been tabulated in Table 23 of Appendix B and f deflection plots have also been included in Appendix B.

l EQUIPMENT HATCH DISPLACEMENTS l The vertical and radial growth around the equipment hatch were l

measured at the locations shown in Fig. 23 of Appendix B. Gage 43V

{

was inspected after the test and found to have been reverse mounted, i causing a sign reversal. This sign reversal has been corrected in this report.

Radial and vertical deflections measured around the equipment hatch were small and in the range normally expected for this region.

The displacements have been tabulated and are shown on Tables 25 and 26 in Appendix B. The deflection plots corresponding to this data is also presented in Appendix B.

i h '

e

-m- u- - -

- -_ _ -w e w_ j i

I l

TEMPERATURE RESULTS Thermocouples were installed at locations shown in Fig. 24 NV \

i of Appendfx C. Table 1 of Appendix C provides actual temperatures -

k

y recorded during the test. The temperatures were normal during the i

s y test with daylight temperature ranging between 75* and 80*, and I' evening temperature ranging between 50* and 65*.

E I

s t CRACK PATTERNS 9 -

The to:a1 structure was surveyed prior to the structural S

jg integrity tes t to reveal cracking which existed. The structure was a

f 1

again surveysd at each pressure level during the test to dete'mine - y a major cracking which may have occurred. The following areas were whitewashed for detailed crack survey: .

1. The discontinuity at the equipment hatch.

2. On the cylinder wall near the base slab on Azimuth 270* Elevation 93'-0".

3. On the cylinder wall at Azimuth 240*, Elevation 172'-0".

4. On the ring beam and dome, a 6 ft wide band starting six feet below the ring beam and continuing to the apex of the dome.

5. Both ends of the twenty-one surveilance tendons. (These were not whitewashed).

Pretest Survey j The pretest survey revealed only minor shrinkage cracks. These l cracks were under 0.005 inches in width and were located primarily in l

l l

l

't

-. ~ - . . . . - - - - - .

, ._ __ :: a -

thickened section of the structure, i.e., bossed areas and buttresses.

The repaired dome showed no visible cracks. The feathered edge in the W

I repaire.i concrete interface with the old concrete was visible but no I,

y cracking could be seen.

a The tendon anchorages were generally free of cracks. Cracks A

which were observed, were less than 0.005 inches with the exception E

1 e of D203F which showed that the construction joint was open crore than t

n 0 0.01 inches.

DEVELOPMENT OF CRACKS DURINC TES"'

S I

A l The cylinder walls remained relatively free of cracks during 8

a i the test. The inspection area at Elevation 172 did not develop any f cracks during the test. The equipment hatch area developed a hairline l

crack at 63.3 psig which closed completely upon returning to atmospere.

l The area at the base slab and cylinder wall intersection developed cracking at 45 psig and had a well defined crack by 63.3 psig. The l width of the cracks were all less than 0.005 inches in width. All I the cracks observed at 63.3 psig closed upon return to atmospheric l l

pressure.

No cracking was detected in the ring beam and wall junction, the )

ring beam proper or the first 14 ft of the dome during the test.

Initial cracking of the dome was observed at 35 psig and appeared as meridional cracks on approximately 24 in centers. At the 45 psig inspection additional meridional cracking had occurred and radial cracks were beginning to fi s. At 63.3 psig a well defined system

. . - . - - n .. ~ u- +_ .- - - - . . - -. a . a - -

I s

of cracks was observed. Meridional crack had a spacing of about 18 ' inches and radial crack spacing was about 24 inches. The majority of cracks observed were measured as hairline, less than i

g 0.005 inches in width. Isolated cracks were observed that exceeded J 0.01 inches for ex*.remely short lengths. One crack on the dome, was a

n n observed to be 0.015 inches in width over a 16 in. length. Upon k.

E:

return to zero the cracks had closed and could not be seen.

I s Appendix D contains detailed crack drawing of the areas e

r inspected. -

a g Tendon anchorage in general performed well. The inspection

{p sheets have been included in Appendix D.

a c

{

SUMMARY

l Interpretation of the data in light of design concepts is not witt.in the scope of this report. However, we feel that a comparison of the response of this structure with the performance of numerous reinforced and prestressed concrete structure which we have observed under many types of test loading justifies the following general commentary regarding the behavior of this structure under the application of the test loading.

1) The overall response of the structure was well substantiated. The displacements observed were uniform between identical points on various Azimuths.

The displacements observed were within predicted values and were typical of displacements measured on other similar structures. The recovery observed e- . , * =%.. , , , , - - , , . . .

. _ - - - - __ _ . . - - _ _ . _ -m._. _ _ . .

., 1) Continued was within limits one would normally expect for a structure 'f this type.

W i

s -

o, 2) Cracking observed on the docte was slightly J

a greater than would normally be expected in a n

~

n g prestressed dome but substantially less and of E a smaller magnitude than could be expected in a a

f reinforced dome. The crack widths (under 0.01 e .

a inches) were such that they did not substantially S increase steel stresses in the dome. The fact that A

s at atmospheric pressure the cracks closed indicated a

i that the structure was still within the elastic f range.

3) The strains recorded for the reinforcing steel were well within the elastic range of this material. This indicates that the structure could undergo more deformation before any significant signs of distress would appear.

Respectfully submitted, WISS, JANNEY, ELSTNER and ASSOCIATES, INC.

Robert Krause f P'?

Assistant Manager of Power Engineering Services T. M. Brown Manager Power Engineering Services RK/TMB/iz

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@ APPENDIX A 1

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I STRAIN DATA l

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3 ELEMENT" SR4 2 DIRECTION AL AtLTECH ELECTRICAL RESISTANCE CONCRETE EMBEDMENT*

STRAIN GAGE STRAIN GAGEE GROUP em.oup 4 enouP a TYPICAL SECTION AT INSTRUMENTATION LOCATION O

EIGURE 14 A-3

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U ROSE 1 t=. GAGE LOCATION ,

INTERIOR. FACE , MAlh' W=AM PENETRATION 9

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FIGURE 15 A-4 1

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4 ROSE i i E GAGE LOCATION INTERIOR. FA"2 f:EEDWATER PENETRA:rlCN 3

e FIGURE 16 A-5

a.---.-.--..- - . . . - . . ... - .-. : .a - -. w ~,a,.:-- a- --

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ROSEiiE GAGE LOCATI ON SPARE PENETRATION ICc=RIOR 3 N

! e FIGURE 17 A-6

-e,. -- --

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\\ 13 7 DISTANCEE. MEEASUEF!D e - INDICKMES A At ONG SURFACEE D - #y STRAIN GAGE OF BulLDING (APROX) [y G R.O U P iso

CONCRE i t= GAGE LOCATIONS AT DOME O

e FIGURE 19 A-8

- -. . . a _.w -.~ m ne~ . - ~ - - . .

~

1 TABLE A DOME STRAIN INSTRUMENTATION Gage No. Radius Azimuth Group Notes Ft Deg.

131 45 75 1 Hoop & merid. reinforcing strain 132 2 Hoop & merid reinforcing strain 133 3 Hoop & merid. conc. strain 134 4 Hoop & merid. liner strain 167 5 Radial anchor strain 135 45 165 1 Hoop & merid reinforcing strain 136 2 Hoop & merid. reinforcing strain 137 3 Hoop & merid, conc. strain' ,

138 4 Hoop & merid. liner strain 169 5 Radial anchor strain

'139 45 255 1 Hoop & merid. reinforcing strain 140 2 Hoop & merid. reinforcing strain 141 3 Hoop & merid. conc. strain 142 4 Hoop & merid. liner strain 168 5 Radial anchor strain 143 45 345 1 Hoop & merid. reinforcing strain 144 2 Hoop & merid. reinforcing strain 145 3 Hoop & merid. conc. strain 146 4 Hoop & merid. liner strain 170 5 Radial anchor strain 148 30 -

75 1 Hoop & merid. reinforcing strain 419 2 Hoop & merid. reinforcing strain 150 3 Hoop & merid. concrete strain 151 4 Hoop & merid liner strain 171 5 Radial anchor strain 152 30 345 1 Hoop & merid. reinforcing strain 153 2 Hoop & merid. reinforcit.g strain 154 3 Hoop & merid. concrete strain 155 4 Hoop & merid. liner strain 172 5 Radial anchor strain 156 15 255 1 Hoop & merid. reinforcing strain 157 2 Hoop & merid, reinforcing strain 158 3 Hoop & merid. concrete strain 159 4 Hoop & merid. liner strain 173 5 Radial anchr strain 160 15 165 1 Hoop & merid. reinforcing strain

'161 2 Hoop & merid. reinforcing strain 162 3 Hoop & merid. conc. strain

, 163 4 Hoop & merid. liner strain 174 5 Radial anchor strain A-9 y s we- p ,

m-- y , .g - , ,

- _ . _ . ~ _ _ . - -

_ . . _ . a_ ; .-_u--~w , .e .- ,~-v_

TABLE B INSTRUMENTED RADIAL ANCHOR LOCATIONS Gage No. Bar No. Radius Azimuth

_ Ft Dez.

167 L30N15 45 75 167* L32R16 45 75 169 L8S4 45 165 169* L6S4 45 165 168 R30S16 45 255 168* R32S17 45 255 170 R8N3 45 345 170* R10N3 45 345 171 L20N17 30 75 171* < L21N18 30 75 172 R6N9 30 345 172* R4N9 30 345 173 R11S19 15 255 173* R12S19. 15 255 174 L3S15 15 165 174* LIS15 15 165

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A-10 y

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Te cI.L 1 EQUIPMENT !!ATCH l'EFIDICt;AL STFAINE (l'ICFOIN./IN. ) ,

i PR ESSURE (PSIC) 0)bo 12.00 35.00 45.00 55.00 63.30- 55.b0 45.00 3b.C0 12.00 0.00

. DATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 TIttE 8.19 18.02 4.04 11.4C 19.11 2. S.25 14.39 19.58 6.00 12.08 CAGE 35M 0 8 82 -31 531 572 541 -74 167 -72 -159 35M* O -3 49 54 118 154 141 41 64 5 . -33 36H 0 -3 13 5 41 46 41 -3 21 3 -8 36t!* O -10 -3 44 -136 -141 -126 51 -36 41- 59 42M* 0 3 33 97 -105 -92 -90 95 -13 49 54 43H 0 -3 15 0 74 90 87 0 36 -3 -15 43M6 0 15 21 23 56 77 79 23 23 23 28

> 43H 0 -3 15 0 74 90 87 0 36 -3 -15 4

e 43M* 0 15 21 23 56 77 79 23 23 23 28 44M 0 -44 -13 26 -169 -149 -133 10 -197 3 -5 i 44H* O -18 -13 21 -146 -149 -136 28 -44 28 49 i 45He 0 -13 3 -3 28 49 54 -23 5 -8 -13 :

46M 0 -33 -23 26 -103 -133 -85 -21 -49 -15 -5 46He 0 -28 8 -8 -26 8 18 -31 -10 5 -8 47M* 0 -23 36 23 74 ' 118 115 -10 31 -5 -33 '

48M 0 13 33 5 138 156 141 -5 46 -8 -33 48Ma 0 -41 5 41 -179 -156 -141 28 -49 28 36 42M* 0 3 33 97 -105 -92 -90 95 -13 49 54 41M 0 21 33 44 77 79 74 38 23 8 3 40M 0 -254 -26 115 -241 -38 -297 138, -505 113 228 40M* O -62 0 36 5 -5 -23 23 -10 '-33 -54 ,

39H 0 -92 -56 0 -95 -95 -95 -3 -72 -54 -56 i 39H* O 21 67 72 118 154 149 67 69 21 0 -

38N O -141 -62 -77 -287 -138 -210 -44 -287 -208 -200 '

3 8tt* 0 -38 -13 69 -115 -138 -146 69 -62 23 33 37H l 0 -74 -44 51 -128 -146 -1 54 36 -197 -195 -87 5 37M* O -5 -23 44 -128 , -151 -167 49 -85 5 31

INDICATES REDUNDANT GAGE

- f

. t

. j TABLE 2 4 ECUIPMENT HATCil HOOP STRAINS (MICROIN./IN.)

PRESSURE (PSIG) 0.00 12 0 35.00 45.00 55.00 63.30 55.00 45.00 35.C0 12.00 0.00 DATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3

. TINE 8.19 18.02 4.04 11.48 19.11 2.41 9.25 14.39 19.58 f.00 12.08 4

CAct !

35H* 0 -15 [

-5 28 -72 -69 -67 15 -33 15 33 36H* 0 21 64 44 172 208 205 38 42H 0 5 13 5 26 31 38 0 92 21 13 -18 r 13 8

. 42H* 0 23 15 0 59 56 59 8 31 3 -8 43H 0 46 97 64 195 246 244 56 126 46 18 4 31t

0 8 46 64 69 97 87 62 51 28 15 [

4 311 0 46 97 64 195 246 244 56 126 l

> 46 18 6 4 3It

0 8 46 64 69 97 87 62

51 28 15 b

N 44H 0 -15 -28 59 -117 -215 -231 69 -77 18 49 4 41t

0 5 13 51 -15 -23 -26 51 0 18 21 458t* O -67 15 18 -110 -56 -46 -38 -44 28 13 4 618 0 -21 10 23 -49 -33 -33 3 -28 8 3 4 61t

O -46 0 21 -95 -79 -85 -38 -87 -44 -54 f 4 711 0 8 18 38 3 3 3 41 5 13 10 4 71t

O -13 46 85 -15 15 10 54 5 31 18 4 811 0 -31 28 74 -82 - 56 -74 41 -18 28 5 4 81t* 0 5 77 56 110 156 141 33 64 23 -15 4211 0 5 13 5 26 31 38 0 21 13 8 4 211* O 23 15 0 59 56 59 8 31 3 -8 4 111 0 72 121 -54' 492 597 595 -36 259 -3 -85 41H* O -13 3 18 -21 -13 -3 8 -3 13 18 d oll 0 -18 -13 10 -67 -62 -62 -5 -33 0 10 4011* 0 -23 -10 13 -59 -62 -56 0 -28 5 8 3 911 0 8 49 49 72 100 100 44 54 21 0 3 Sit

0 -59 -31 33 -126 -118 -118 13 - 77 -15 0 3 ell

O 41 154 174 246 331 295 167 156 62 10

' 11 0 -146 -103 62 -338 -354 -374 41 -213 -62 -28 s ,Jit

O 292 359 405 41 256 231 41 51 -69 -118

INDICATES REDUNDANT CACE

?

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- t t

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' MAIN STEM: LINC PC:.LTIt71C:2 E1rtit.0 (rlCFCIt../I:;.) '

, PTCSSUPC(PSIC) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.C0

l GATE ' 10/31 10/31 11/1 11/1 11/1- 11/2 11/2 11/2 11/2 11/3 11/3

.i t ir.:n 8.19 18.02 4.04 11.46 19.11 2.41 S.25 14.39 19.58 6.00 12.00 CACC I

76tt 0 -110 -87 -63 -7 3 -23 -63 0 -80 -77 76c 0 -113 -140 -133 -97 -100 -123 -150 -1C7 -117 -63 l 76M 0 -10 -17 40 S7 120 100 57 13 -73 -47 77H 0 -37 .377 207 293 31 7 293 233 377 127 . -40 770 0 3 100 120 163 180 160 130 123 C3 7 i

-77tl 'O -87 -30 -33 ' 17 23 -3 -33 93 -27 -90 !

78H 0 -27 -23 -17 -3 10 -13 -30 -43 -37 * -10

. .700 0 -33 17 43 90 110 70 37 43 -

-40 i 7Ct1 0 -7 -3 40 07 120 57 3 -57 -53 -23 7 911 0 13 163 .200 260 290 273 220 267 137 30 p 790 0 1000 667 1000 667 C67 333 Ef7 667 667 667 1 79M 0 27 70 67 70 63 57 63 37 30 30

,U 8 011 0 -60 -20 -20 23 40 20 -17 60 -10 -67 I 80D 0 -37 13 23 57 70 53 20 73 7 -50 00:1 0 3 47 CC 77 C7 73 57 53 17 -7 i 4

C111 0 -47 0 3 53 67 50 13 77 3 -60

810 0 -20. 20 30 57 63 47 27 53 7 -33 81M 0 -3 SC -130 -C3 33 20 10 17 -C3 -73 t 0 21 0 -3 53 77 110 123 100 77 C7 67 20 i 82L 0 3 57 C3 101 117 103 LO 90 37 -7 d 8 2tl C 0 -333 0 0 0 -333 0 0 0 6 i 8 311 0 -667 -333. -333 -1000 -333 -667 -333 -333 -667 0 830 0 - 333 -333 -667 -667 -667 -667 -667 -333 -667 -667 8 371 0 -667 -333 -333 -333 -667 -667 -667 -333 -333 -333 84H 0 -333 -667 -667 -667 -333 -667 -667 -333 -1000 -667 840 0 -333 -667 -333 -667 -667 -667 -333 -333 -333 -1000 84M 0 333 0 0 333 -333 -333 333 333 0 0 8 541 0 0 -333 0 -333 0 -333 -333 0 -333 0 850 0 -333 -333 -333 -667 -667 -667 -667 -667 -667 -667 8 5M 0 0 0 0 -333 -333 0 0 333 0 -333 4 0611 0 -333 -6G7 -667 -1000 -667 0 -667 -333 -667 -667 86D 0 -333 -333 -333 -333 -333 0 -333 0 -333 -333 l 8 614 0 -667 - 333 -667 -667 -333 -667 -667- 0 -667 -667

. 8 711 0 0 0 0 0 -333 -333 0 0 0 -333 870 0 333 -333 -333 .133 -333 0 -333 -333 0 -G67 87t: 0 0 -333 -333 -333 0 -331 -333 -667 -333 -333 -

88H 0 -333 0 -333 -333 -333 -667 -333 0 -233 -667 4 08D 0 0 -333 -667 -333 0 -333 -333 -333 -33J -333 I-8Cr: 0 -333 0 0 -333 -333 -333 0 C -333 -333 l 8 Eli 0 -333 -333 -667 -333 -333 -333 -607 -667 -667 -667 [

i 890 0 -333 -333 -333 -6f7 -333 -667 -333 -333 -333 -667 6 89M 0 -333 0 0 0 0 0 -333 0 -333 -667 I

I e

I t-1AELE 4 FEEDt!ATER LINE PENE11'ATIOh STFAINS (E ICTOIti./IN. )

r

==--- - ______- .. . .__.______ _ ______. I PR ESSURE (PSIC) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00 l EATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 i ilt:E 8.19 18.02 4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.ce t.

- - . : == _ . .

CACE-9 011 0 -667 -333 -667 -667 -1000 -1333 -1000 -667 -667 -1000 900 0 -667 -1000 -667 -1000 -667 -667 -667 .-667 -667 -1000 9 21 0 0 -333 0 0 0 0 0 0 0 -333 9 111 0 -333 0 -333 0 0 333 0 0 0 0 '

91D 0 333 0 0 -333 -333 333 0 333 0 -333 '

91M 0 -333 -667 -1000 -667 -667 -567 -333 -333 -333 -667 ;

9 211 0 0 -667 -667 -667 -333 -333 -667 -333 0 -667 920 0 -667 -1000 -667, -667 -667 -1000 -G67 -667 -667 -10C0 92:1 0 -333 -667 -667 -1000 -1000 -667 -333 -667 -667 t 9 318 0 - 333 0 -333 ~333 -333 1333 -333 -333 -667 -667-

>e 93r 0 333 0 -333 0 333 -333 0 333 0 0 94 0 333 -333 -333 0 -333 -333 -333 333 - 333 -667

'$ 940 0 -50 17 7 33 53 40 13 63 3 -60 94N 0 -27 43 43 77 90 73 47 93 27 -33 9 511 0 -33 37 40 63 03 70 47 97 27 -33 .g 95D 0 -33 97 100 137 153 140 120 167 103 33 -

95M 0 -27 33 40 67 87 70 47 90 17 -37 1

.96I1 0 - 333 -667 -667 -667 -667 -667 -667 -333 -333 -667 96D 0 -333 -333 -333 -667 -333 -333 -667 -333 -333 -333 96M 0 0 -333 ,333 -333 -1000 -667 -667 -1000 -1000 -667 970 0 0 -333 -6G7 -667 0 -667 -667 0 -667 -333 9 7tt 0 0 - 333 -333 -333 -333 0 -333 -333 -333 -333 9 611 0 -333 0 0 0 0 0 -333 0 -333 -333 900 0 -667 -667 -667 -333 -667 0 -333 -333 -667 -667 9 Ett 0 -667 -6G7 -667 -667 -667 -667 -1000 -333 -667 -1000 9 911 0 333 0 0 0 0 0 0 333 0 0 990 0 -333 -667 -667 -667 -667 -G67 -GC7 -667 -667 -667 99?1 0 -333 -661 -667 -667 -667 -667 -667 -1000 -667 -667

-20011 0 -333 0 0 -333 -333 0- -333 0 -667 -333 100D 0 667 667 -1000 -667 -333 0 -667' -667 -333 -333 100tt 0 333 333 0 0 333 333 333 0 0 0 i

. 10111 0 0 -333 -667 -333 -333 -333 -333 -333 0 0 1010 0 -667 -1000 -667 -667 -333 -667 -667 -667 -667 -667

. 101M 0 -333 -667 -333 -333 -667 -333 -333 0 -333 -333 102il 0 0 -333 333 0 333 667 0 333 0 0 162D 0 -667 -667 -667 -667 -333 -667 -667 -333 -667 -667

102M 0 57 23 -47 -33 50 20 0 20 -7 -37 i 1031t 0 -333 0 -333 -333 0 -333 -333 0 -333 -333

103D 0 0 -333 -333 -333 0 -333 -333 -333 -333 -333 f*-

Z I

i .

^

l f

TABLE 5 SPARE I ENETRATION STRAINS (MICROIN./IN.) g

_ _ _ _ _ _ _ _ _ _ _ _ _ . - . _ _ _ _ _ _ _ _ _ _ _ = = - -

I'RESS URE (PSIG) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00 !

DATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 flIME 8.19 18.02 4.04 A1.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08 CAGE 104H 0 -333 -333 0 0 -333 -333 -333 -333 - 333 ' -667 104D 0 -333 -333 -667 -333 -333 0 -333 -333 -333 -G67 104M' O - 333 -333 -667 -333 0 -333 -333 -667 -667 -667 10544 0 0 -333 0 -333 -333 -667 -333 -333 - 333 -667 105D 0 -667 -667 -333 -667 -667 -667 -1000 -667 -1000 -1000 105M 0 -333 -333 -333 -333 0 -333 0 0 -333 -333 106D 0 57 113 137 150 147 143 133 90 60 60 106M' O -87 -37 -27 10 50 30 0 77 0 -83 107H 0 -27 30 50 70 83 73 63 87 43 3 107D 0 -7 43 63 87 103 93 73 73 23 -17 108H 0 -23 30 50 73 97 83 60 83 30 -13

> 1080 0 27 67 77 107 110 113 117 80 77 70 8 108M 0 33 77 97 113 113 107 100 67 43 37 Ui 109H 0 -47 13 27 57 83 63 40 80 3 -63 ,

, 109D 0 -123 -63 -53 0 37 10 -27 90 -17 -127 .)'

109M 0 -40 10 23 47 63 53 33 73 23 -27 110H 0 -137 -33 -13 57 117 70 13 153 -10 -160 110D 0 -50 -7 0 27 47 37 20 77 20 -43 110M 0 -153 -70 -63 -7 50 13 -37 117 -23 -173 5 111H 0 -53 27 40 83 113 80 43 80 -10 -110 111D 0 -20 20 23 37 43 33 30 47 27 -3 111M 0 -93 3 0 37 83 43 3 100 -7 -123 112ll 0 -57 30 60 107 143 110 67 127 3 -93 1120 0 -37 -13 -10 -3 7 -3 -13 27 -7 -43 112H 0 -90 -3 17 77 107 83 53 137 30 -50

. 11311 0 -20 70 93 133 170 147 110 133 30 -47 113D 0 -113 -100 -137 -90 -53 -83 -103 27 -60 -140 113M 0 -27 13 20 33 47 37 20 50 0 -40 114H 0 -10 80 103 143 173 147 110 127 30 -40 1140 0 -143 -73 -83 -33 0 -27 -60 93 -43 -157 114H 0 -57 -10 -3 27 43 23 0 57 - 33 -107 115H 0 -20 67 87 127 157 137 100 133 37 -33 115D 0 -47 10 13 37 40 37 23 83 27 -27 115M 0 -23 30 40 67 87 77 60 90 30 -10 11611 0 -3 70 93 130 150 ' 130 107 113 43 -13 1160 0 -20 3 7 23 27 23 17 43 13 -10 11611 0 -1C7 -33 -43 7 43 13 -23 100 -2C -130

, 11 31 0 3 60 1C0 130 150 133 113 117 47 -7 117D 0 -57 -10 -20 7 13 -7 .-33 30 -47 -117 117M G -53 23 30 ?O 107 EO 53 120 20 -53 i

TALLL 6 6

CYLINDER UALL 1.ND LCIT. JLACTICH IEEIDICEAL STFAIhS (f.ICF CI b .*/It. . ) l AzIt:U1u 90 ,.

e PRESS URE (PS IC) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.C0 12.00 0.C0 !

LATC 10/31 10/31 11/1 13/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 j TINC 8.19 18.02 4.04 11.46 19.11 2.41 S.25 14.39 19.58 6.G0 12.05

_ _ _ _ _ _ = _ _

t CACC 70et 0_ -27 -10 -3 30 50 30 7 43 -33 -93 73H 0 -57 -3 7 SC 53 50 50 97 43 -7 4 9tI* 0 15 82 115 -54 G 3 74 -10 -31 IL 52r; O 49 -62 -90 -40C -367 -4C5 -154 -352 -62 -96 52E* 0 -18 54 56 -26 le 23 3 -10 13 3 55?: 0 -28 -103 -1C -454 -410 -405 -10 -465 b -3 55r1* O -44 15 103 -110 -105 -105 57 -49 54 51 SSM* 0 44 82 97 12C 146 128 100 92 46 28 61H 0 -16 -26 -49 30 3G 2315 2531 2661 2455 2523 61H* O 10 -5 -5 23 18 23 E 13 -21 36 ,

64tt 0 26 215 2G5 328 346 331 303 197 -503 64 Y 64H* 0 0 0 0 0 0 0 0 0 o' 0 I-H 67M 0 0 0 0 0 0 0 0 0 0 0 i

67H* 0 -18 54 59 -6 31 51 -13 -2C 8 -3

[

INDICATES REISUNDAN1 CACE I

2

.L. s 4

f f

s f

!~ .1ALLC 7 CYLINCEP t' ALL AND LCML J0tiCTICle ELTID10hAL ST EAlt.S (t.ICECI A .'/IN . )

A11hb11. '200

. t-

-- - .-- - -- ....____ _ .._ . t PEESSURC (PSIG) 0.00 -12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.C0 #'

- CATE- 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 -h" 11HE 8.19 18.02 4.04 11.4C 19.11 2.41 S.25 14 39 19.58 6.00 12 S s

C GACE y o

I 71st 0 -3 33 43 70 80- 70 63 to 30 7 P 74t: 0 -27 20 43 C7 100 90 SC 143 57 -10 50:.I 0 -10 72 62 69 126 105 31 49 31 -10 56ti* O -21 49 13 3 54 36 -44 -31 0 -31 ;

53H 0 -13 46 8 10 51 44 -23 5 23 3 ((

53H* 0 -33 64 -21 5 67 26 -62 0 21 -36 L 5 61:* O 38 95 133 149 102 162 133 108 46 15 '

S SM

O IC 105 110 141 174 138 105 90 23 -18 l

> . 62H* O 62 192 231 282 341 202 236 162 44 -1E $

u GSM 6 56.*

0 0

60M 0 5 31 18 -10 3 13 -10 -20 -10 5 6 8ts* O -36 13 5 -33 -13 3 -36 -13 -10 -22 4 4

INDICA 114 'i.f J:!6 f ?NT CACE r

L 9

e

?

t t.

?

- - -J

t i .l~

T.-

1AbLE 6 CYLINDEP KALL FND LCFC JLEC110td I EFIC10t;7L STF71!.C (t. IC TC1t; .~/lta . )

A'4IF U114 333-55 ~

.- --- _____ ..._____ y ERCSS URE (ESIG) - 0.00 12.00 35.00 45.00 SS.GG 63.30 55.00 45.00 35.00 12.00 0.00 10/31 10/31 11/1 11/1 g'.

CAT E 11/1 11/2 11/2 11/2 11/2 31/3- 11/3 1It:C 8.19 10.02 4.04 11.40 19.11' 2.41 S.25 14.3S 35.50 6.CC 12.C8

-- --- == -- - - - ..._... ___.....____________......___..--- _

i s

C/CC '

f r

7 21: -0 -17 1C 20 40 40 33 3G 47 17' -10 'h' 75r 0 -67 -133 -133 -133 -100 -100 -133 -100 -ICC -67 t 5 12. 0 31 300 11C 100 141 12C 15 67 44 21 512:* ~0 2C 151 164 167 22 G -]S2 1CC 121 54 -C ?

54t: 0 13 10 72 31 15 4G -44 -2C' -100 -104 54tia 0 2G 103 100 05 121 1C5 40 51 30 10 5 711

O 46 144 20C 23C 236 245 235 ISS 57 56 .

Gmt 0 33 C7 115 13G 162 14C 126 f2 3C 13 5

> 60 !* O 38 115 149 17S 210 105 154 121 4S C h

C 3i:* C CS 107 22C 202 392 302 3CC 244 136 C5 '

0G:: C 0 0 0- C 0 0 C C C C C C::* O 43 144 107 236 267 220 ISC 14S 44 -3 GTt:* 0 0 0 0 C C C C C C C

!!JCICATES F.ELUhC7141 CACC F'

r b

4 ,

p L'

t i .

i t b.

Ip 4

4 e

, i 1

i

I-

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t.

TAELI C 7t

. CYLINDtc UtLL 7t:C Cct t jct:C11Ct 1.CCI E10AlleS (l' ICt CI t' ./I t!. )

7215 U11: 50 ,

. p

k. ,

FREECUTC(PSIC) 0.00 12.00 35.00 4h 00 55.00 63.20 55.00 45.00 35.00 12.00 0.0C '

[.AT E 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 TI!4C 8.19 10.02 4.04 11.48-- 19.11 2.41 S.25 19.58

_ = -

=- ____

14.3S . 6.00 12.08 3 CACC s

7c!! 0 -140 -73 -c7 -7' 30 -23 -70 c3 -63 -170 73:1 0 33 100 130 177 197 300 160 133 C3 23 4 Sit 0 110 22C 150 221 287 256 177 95 51 0 4 9II* 0 -23 123- 131 54 144 133 49 44 31 -3 5211 0 -28 62 30 -5 49 30 -I C 0 10 -15 52 t1* 0 3 87 69 21 74 GS 13 -3 i.

-56 5 55:I* 0 0 -256 -256 513 256 0 513 25G4 513- 1026 ,

SGli C 0 -30 -51 -51 -69 -5T -31 -31 -3 10 T

5 811* O -8 -49 -33 -2S -46 -30 -5 -23 2C '44

611!* 0 62 185 241 310 354 315 274 213 c5

31 G 411 0 0 0 0 0 0 0 G 0 - 0 0 64 tl* 0 -3 -5S -64 -67 -07 -72 -33 -36

-10 15 -

67tl 0 0 0 0 0 0 0 0 0 0 0 G 711* O O O O O O 0 O O 0 0

INDICATES REDUNDANT CACC 1

r I. -

h e

. ?

4 l'

. TJ. ELE IC 'I 1

CYLINLET t:1.LL AND DCS E. JLhC11Ct. I:CCP S1F Alle: (b.1CTCIh . /Ilv . )

AZIt!Ul t! 200 kI p

PRESSUCE (PSIC) 0.00 12.00 35.00 .45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00 L DATE 10/31 8.19 10/31 11/1 11/1 11.4C 11/1 19.11 11/2 11/2 S.25 11/2 14.39 11/2. 11/3 11/3 )'

71t+C _

18.02 4.04 2.41 19.58 .6.00 12.Ce 5

CAGE L. ,

71It 0 333 667 333 -333 -667 -1000 -1667 -1333 -2333 .-2666 74 pt 0 -10 73 110 180 207 173 150 180 37 -43 5 011 0 -36 69 8 -3 64 21 -100 -62 -46 -118 i 5 011* O -3 103 59 77 149 118 18 33 3C -5

53tl 0 -618 -867 -367 -638 -674 -438 -508 -679 -669- -526 t 53!!* 0 -15 .49 13 21 64 28 -21 C 18 -15 56ft 0 -28 -44 -62 -5G -62 -67 -54 -1C -2G -38 56t!* 0 -3 -44 -44 -49 -67 -56 -31 -31 -5 13-Y 596t

O -5 -49 -51 -56 -67 -64 -36 -21 3 23 N -209 6281* 0 -44 -151 -118 -154 -182 -182 -130 -174 -140 6 511 0 0 0 0 0 0 0 0 0 0 0 651t

0 -10 -72 -69 -82 -100 -77 -44 -46 -c 13 G Bil 0 0 0 0 0 0 0 0 0 0 0 6 811* 0 62 82 138 77 123 102 10 33 '4 C2 i

,

INDICATES ECDUNDANT CACC f

i e

1 i

I t

b k

e i;

f P

f '

f I

a

~

i i

1ACLE 11 l}

i _.-__--____ .

CYLINDER WALL AND DOME JbtJC11CN liGCP S1PAIkS (M ICFOIN .'/IN . )

A ZII;U's !! 333-55

'i

. PPESSURC(PS C) 0.00 12 00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 -12.00 0.00 , CAS E 10/31 10/31 11/1 11/1 11/1- 11/2 11/2 11/2 .11/2' 11/3 11/3 11HC 8.19 18.02 4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08

                                                                              ==                     _=         _                   _-.   ----..._        ___ -_

j CACC 72I1 0 -37 27 43 97 117 87 50 80 -7 -47 75I1 0 -S0 -103 -113 -83 -80 -97 -107 -33 -67 5111 0 23 95 C7 C5 118 97 46 51 21 -5 5111* 0 54 167 172 131 105 172 69 G4 54 21 Seit 0 36 95 318 13 192 231 131 172 95 41

 '                                                        5 411*                   0-    36      131      123               79     126            113       36      36     44    3C 5 711                    0    -15      -44      -56              -59     -64            -64    -51      -28     -15                                                              5 7tl*                   O     26       54      -41              -51     -64            -72       44      21      3   -13 6 011                    0     28     -100    -118             -130     -102          -126   -102      -141     -49   -E2          ,-
             +4                                           601t*                    0     -8      -51      -51              -62     - 74          -62     -3C      - 31     -5    13          i e-.                                    6 3tI*                   O    -10      -62      -74              -E5    -105           -e7     -51      -54     -10    21 6 611                    0   -256     -256     -256              256          0         256    256      256     256     0 6 6II

0 -21 -69 -C5 -82 -90 -77 -46 -36 -8 13 6 911 0 0 0 0 0 0 0 0 0 0 0 6 9tl* 0 0 0 0 0 0 0 0 0 0 0
INDICATES REDUNCANT CAGE

. -? u ! . (- 1 t i

                                                                                                                                                                                             .t r

s

w,O

                                                                                                                                                              }  r p

i 4 TABLE 12 : ________ - 1

                                                                                          !                                                                      t
,                                                                    WALL LINER STRAINS (MICROIN./IN.)                                                              E i               P'R ESSURE (PSIC)          0.00       12.00       35.00       45.00               55.00  63.30    55.00       45.00     35.00   12.00   '0.00

DATE 10/31 .10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 k

. TIME 8.19 18.02 ~4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08 !

_ _==. = =

GAGE A3. -ELEV. 70H 90 172-0 0 -140 -73 -87 -7 30 -23 -70 83 -63 -170 70D 0 -73 -37 -37 13 33 3 -30 47 -57 -113 70M 0 -27 -10 -3 30 50 30 7 43 -33* -93

.(

3 71H 200 172-0 0 333 667 333 -333 -667 -1000 -1667 -1333 -2333 -2666

710 0 -7 63 53 87 100 77 53 67 -3 -37 t' 71H 0 -3 33 43 70 80 70 63 80 30 7 i

Y 7211 333-55 172-0 0 -37 27 43 97 117 87 50 80 -7 -47 PJ 720 27

      "                                      0        -47            3            10                50    70        50                   73       0     -43 72H                          0        -17           10            20                40    40        33          30       47      17     -10 4

j 100 l 73H 90 204-0 0 33 130 177 197 180 160 133 63 23 t'

l. 73D 0 -33 27 40 97 117 93 70 120 13 -50 4

73M 0 -57 -3 7 50 53 50 50 97 43 -7 , 74H 200 204-0 0 -10 73 110 180 207 173 150 180 37 -43 74D 0 -83 -3 17 90 117 77 50 177 0 -117 l 74M 0 -27 20 43 87 100 90 90 143 57 -10 1 4 ' 75H 333-55 204-0 0 -90 -103 -113 -83 -80 -97 -107 -33 -67 -70 ! 750 0 -93 -60 -60 -7 20 37 43 183 103 67

;               75M                         0         -67        -133        -133                -133   -100     -100        -133      -100   -100      -67 i

p 4 4 l 1 4 I

                                                                                                                                                                'I ir

P s ki j V TACLE 13 DOFE MERICICNAL STFAINS (MICPCIN./IN.) FADIUS 45 fLET

      ' PR ESSURE (PSIC)         0.00             12.00  35.00    45.00        55.00       63.30    55.00     45.00     35. 00      12.00                       0.00 DATE                  10/31               10/31    11/1     11/1         11/1        11/2    11/2       11/2       11/2      11/3                       11/3                          f, '

TIME 8.19 18.02 4.64 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08 ___- __. _ _ _ _ . _ - - - - = = _ _ - - _.-= - ..... GAGE AEIttuTH 75 131M 0 -24 -272 -279 -77 -292 -146 115 162 -90 253 131M* O -23 -121 -155 -145 -200 -183 -104 -100 8 132M* 0 -1 73 87 62 74 78 51 28 13 0 134H 0 7 -3 7 27 37 37 37 7 -10 3 AEIMUTH 255 139M 0 32 281 281 336 487 400 229 222 119 35 J 139M* O 27 109 114 115 255 227 126 128 83 28

> 140M 0 29 163 212 228 358 321 217 176 99 49 1

140M* 0 28 113 150 142 236 223 155 124 73 36 U 142M 0 7 3 13 33 40 40 47 23 13 10 I A11Mu1H 165 5 e 135M 0 13 117 112 92 137 127 49 51 21 -29 135M* 0 -3 105 112 81 144 138 49 55 31 -27 136N O 26 109 123 109 136 126 81 51 9 -23 136M* 0 14 96 119 105 136 128 81 51 17 -18 138M 0 80 120 157 153 167 170 173 87 100 213 AEIMU7H 345 t 143M 0 -37 -259 -277 -290 -414 -377 -274 -206 -105 -54 h 143H* O -40 -115 -227 -323 -562 -491 -304 -267 -154 -67 144M 0 38 131 131 129 158 142 72 67 23 -37 144M* O 41 117 140 136 162 147 105 74 24 -18 146M 0 37 97 117 137 167 153 140 97 53 50 L t

INDICATES REDUhDANT CAGE b L

e ,

?-

4

i 1

                                                                                                                                                                                                                         !i.~

( t i- !

                                                                                                                                                                                                                        -t TABLE 14 DOME MERIDIONAL STRAINS (MICROI N ./IN .)

RADIUS 30 FEET __.________________ = = _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ - - = = - - - _____________________-- = PR ESSURE (PSIG) 0.00 12.00 35.00 45.00 *5.00

                                                                                                                ,         63.30            55.00           45.00       ~35.00              12.00              0.00 DATE                .10/31             10/31               11/1           11/1                 11/1     11/2             11/2             31/2         11/2                11/3            11/3 TIME                    8.19           18.02               4.04         11.48               19.11        2.41            9.25           14.39        19.58                G.00            12.08
                                                                         - - - = - .                 ==______-            =_______________________________                               ___________________             g F
!                  GAGE                                                                                                                                                                                                  I-l AZIMUTH 75 i                  148N                      0                        38      499            538                  636      794              676              395          346                126               -9 148H*                     O                    -33         387            360                  322       533             460                79         -10              -151              -251 149H                      0                        14      129            212                  209       265             249              179          135-                  79             46 149M*                     O                        36      218            315                  346      442              408             317           251                141               79        L 151M                      0                        60      117            160                  190      217              210             207           140                127              120      -1 I
            >e y                              AZINUTH 345                                                                                                                                                                   j 152M                      0                    -96      -453           -509                 -554       -617            -570             -4 74        -349               -109                18 152M*                     O                    -47      -628           -724                 -877      -1049            -872             -549         -440               -177               -45 153M                      0                        65        63           264                  545      399              271              686          758                458              483 153He                    -0                        37     232             267                  290      364              344              276          231                127               67        I.

154M 0 -37 0 -13 10 13 -3 -20 43 -17 -70 155M 0 47 103 147 173 193 183 163 100 63 53 .-. t

INDICATES REDUNDANT GAGE i 1 i

l-F t.. l-E y t-

                                                                                                                                                                                                                        .h a

4

.}

I p., k6

                                                                                                                                                      >   i
                                                            . TABLE 15                                                                               1 DCHE MERIDIONAL STRAINS (MI CROI N ./I N .)

RADIUS 15 FEET

                                  ==                             -
       . PRESSURE (PSIG) -    0.00     12.00   35.00    45.00      55.00            63.30         55.00        45.00       35.00   12.00   0.00 DATE                10/31     10/31    11/1     11/1        11/1             11/2         11/2          11/2       11/2    11/3   11/3     - 'l TIME                 8.19-    18.02    4.04   11.48       19.11              2.41         9.25        14.39       19.58'   6.00  12.08      I

_-_--- -_ __ - --------__ =_ 1 L CAGE ' AZIMUTH 255 ' 156n 0 29 108 108 92 118 112 46 46 15 -31 156M* O 23 83 73 73 182 176 71 106 lb8 56 . 157M 0 -28 -118 -195 -201 -258 -244 -179 -131 -64 -27 , 157M* O -32 -117 -218 -219 -294 -279 -217 -162 -85 -47 158N O -20 57 87 117 137 120 83 127 20 -50 p 159H 0 33 120 160 213 253 230 197 163 73 30 i 84 ASINUTH 165 1 160H 0 -18 -123 -124 -112 -205 -190 -91 -88 -40 15 i ! 160Ma 0 -19 -81 -376 -399 -533 - 56 -221 -186 -85 -14 l 161H 0 -31 -117 -150 -158 -237 -2'44 -174 -128 -72 -36 161M* 0 -40 -121 -415 -426 -520 -463 -326 -209 -74 -21 162M 0 -7 0 -3 0 -3 -3 -3 17 -7 -23 1 163M 0 2913 -1766 -1357 -857 -823 -820 -847 -1470 -1037 -1000 l 4

INDICATES REDUNDANT CAGE 4

I i L p w 4

.,~

r TABLE 16 {I DOME !!OOP STRAadS (MI CROI N./I N . ) j-RADIUS 45 FEET PRESSURE (PSIG) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00 DATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 TIME 8.19 18.V2 4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08 _-----------.........-- ...==-- _ - . . - = - - - - - - = - - - - _ - - - - -

      ' CAGE AEIMUTH 75                                                                                                                                         f t

131H 0 18 -86 -77 -49 -108 -96 -13 -28 -13 23 1311t

0 6 -87 .-86 -54 -79 -82 -24 -29 -17 15 l 132H 0 -31 -131 -164 -151 -185 -172 -117 -85 -35 5 l 132He 0 -33 -141 -162 -162 -199 -176 -121 -79 -19 19 '

133H 5 -17 0 -7 -3 3 -7 -17 10 -7 -33 134H v -7 40 73 127 163 137 110 93 13 -20 AEIMUTH 255 i f-b C" f 139H 0 6 131 117 126 242 200 95 105 67 14 ! 139H* 0 3 101 74 79 94 83 14 32 19 -13 t 14011 0 24 136 153 169 215 183 129 105 50 17 k 14011* O -4 47 58 46 53 58 19 5 -1 -19 1 141H 0 -73 -50 -67 -43 10 -60 -73 -100 -140 -113 142H 0 -60 63 87 187 230 180 123 220 47 -37 AEIMUTH 165 e 135H 0 -29 260 218 245 346 285 82 115 72 -12 135H* O -24 171 209 200 305 281 141 150 109 44 136H 0 -13 187 247 218 297 281 IG8 118 72 40 136lt

O -9 86 197 1 77 259 250 165 114 67 36 137H 0 -43 40 47 73 103 70 40 87 0 -67 l

13811 0 23 137 177 240 280 250 210 203 97 43 Y AEIMUTH 345 b t 14311 0 -33 -59 -38 -35 -59 -37 -22 -41 -19 3 h 143H* O -14 -74 -96 -82 -104 -101 -71 -42 -15 1 F 14411 0 14 358 336 372 .453 385 222 204 .18 58 k 144H* O 15 304 354, 355 427 382 249 186 104 64 ); 145H 0 -37 20 50 67 83 63 33 87 3 -53 ? 14611 0 -37 83 113 197 243 203 137 20 0 50 -50 if

INDICATES REDUNDANT GAGE

r

<}.

1 TABLE 17 g f DOME HOOP STRAINS (MICROIN./IN.) RADIUS 30 FEET PRESSURE (P SIG) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00 DATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 i' TIME 8.19 18.02 4.04 11.48 19.11 2.41 - 9.25 14.39 19.58 6.00 12.08 { _==_ _ = -. - _ _ = = = _ - - - - - _ _ - - - - _ _ = = = - - _ . _.. _... .. ----- CACE p A3IMUTH 75 [;. 6 14811 0 -22 -Ir/ -168 -213 -351 -310 -167 -182 -103 -12 k-148H* O 0 .4 -372 -353 -431 -355 -146 -151 -47 45 14911 0 -26 -326 -442 -465 -605 -546 -378 -278 -124 -47 1 14 91t

O -40 -286 -363 -395 -483 -442 -327 -245 -103 -35 L 150tf 0 -50 ' -40 -37 -27 -13 -20 -33 20 -27 -77 !

y 15111 0 13 103 137 193 227 217 197 197 133' 90 i AEIMUTH 345 l s 15211 0 35 345 404 509 612 495 288 '265 112 6 152tt

O 27 210 244 308 420 353 182 163 68 -15 .?

t 15311 0 55 381 518 585 606 583 624 553 426 368 153tl* 0 31 324 459 508 632 560 383 274 122 55 15411 0 -17 43 50 67 77 63 47' 73 3 -40 - 155I1 0 -3 60 93 133 170 153 133 127 50 10 f,

INDICATES REDUNDANT CAGE Il f

.t?

fi i y: (.i b s e

G g. TABLE 18 l DONE HOOP STRAINS (MICROI N . /IN .) RADIUS 15 FELT [ 1.__.___. .. --

                                                            -_-           .__..         ===--- ___... _ ...____                              _ . _ . . . . . _ . _ _ . _ _ . . . . . . . . . _ _ _

PR ESSURE (P SIG) 0.00 12.00 35.00 -45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00 DATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/1 '11/3 1 TIME 8.19 18.02 -4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08 4 - _ = - - - - _ _ ___ - _ =_ _ -=.-- =-- - -__ =- _ - - - - ____- --_

        'CACE A3IMUTH 255 4

1 56l1 0 -18 -227 -222 -251 -321 -274 -127 -122 -60 -3 156n* O -33 .-106 -113 -123 -164 -155 -85 -94 -59 -4 157H 0 36 -50 68 88 79 68 72 42 -26 -55 i 1571t* 0 27 126 162 162 194 188 146 119 77 45 i

+         158I1                      0                  -20             10              0              10                 17        7    -13              40               -7              -60          4
     >s   15911                      0-                  43            120        160                207                 240     223     203            160                87                57 N

co A3IMUTH 165 &- p i ! i 160H 0 -12 -97 .35 -114 -205 -201 -109 t

                                                                                                                                                      -103                -59                -4        .{

160H* -91 -194 O -32 -135 -115 -210 -97 -92 -45 6 i' 16111 0 -27 -183 -265 -294 -400 -369' -276 -195 -90 -44 161H* O -36 .-99 -151 -149 -237 -227 -173 -121 -63 -29 16211 0 -33 -30 -33 -20 -20 -30 -37 7 -30 -70 16311 0 37 113 150 217 280 337 323 280 467 487 b- . i l.

INDICATES RECUNDANT GAGE p-4 V

;                                                                                                                                                                                                       p 6

5-5' t' 7 L I'I c,

l

                                                                                                                                    ,    '!     .i b

i i l TADLE 19 I-5 i5 DOME RADIAL STEAINS (MICECIN./IN.}

                  .                                       RADIU9          45         FEET                                                  I.

_ _ _____ _ _ _ _ _ - - _=_- 0.00 12.00 35.00 PRESS URE (PSIC) DATE 10/31 10/31 11/1 45.00 11/1 55.00 11/1 63.30 11/2 55.00 11/2 45.00 11/2 35.00 11/2 12.00 11/3 0.00 11/3 [ TIME 8.19 18.02 _ 4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08 I GAGE L t AZIMUTH 75 167R 0 8 27 18 23 28 27 18 13 22 35 167R* O -2 12 8 10 10 10 12 13 -168 -152 1' I i y ASIMUTH 255

e , 168R 0 3 -3 -7 -8 -5 2 5 -7 13 27 168R* 0 0 2 3 12 13 25 38 72 95 105 AZIMUTH 165 169R 0 -12 -30 -32 -40 -43 -38 -30 -20 -7 -2 169R* 0 -18 -15 -23 -15 -12 -17 -18 -10 -8 -2 AZIMUTH 345 is t 170R 0 8 -5 -2 -17 -22 -7 3 -13 15 32 170R* 0 -8 12 27 28 62 83 75 60 77 82 L

INDICATES REDUNDANT CACC i L.

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TABLE '20 ( DOME RADIAL STRAINS (MICROIN./IN.) RADIUS 30 FEET i . - - - - . - - - - - - - - - - - - - . _ _ _ _ _ . . . . . . . - - . . - - - - - - . . .. -----= - - - . - - - - . . . - - - - - - - , - - - - . PRESSURE (PSIG) 0.00 12.00 35.00 45.00 55.00' 63.30 55.00 45.00 35.00 12.00 0.00 ' DATE 10/31 10/31 11/1 11/1 11/1 11/ 2 11/2 11/2 11/2 11/3 11/3-TIME 8.19 18.02 4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 t2.08 _ l

-t

! cacE .f-ARIHuTII 75 171R 0 -22 -25 -25 -28 -20 -12 -12 7 33 42 171R* 0 .-13 -22 -23 -33 -32 -25 -20 -15 5 12 l ARIMU1H 345 b o 172R 172R* 0 -3

80 12 18 O 103 113 t-

INDICATES REDUNDANT CACE E

4 i-L

                                                                                                                                                                                                                      's
                                                                                                                                                                                                                 . E v.

l h-E o G. E-

i.~ - TABLE 21 DCHE RADIAL STRAINS (NICROIN./IN.)

                                                  ,                                                                                      RADIUS       15      FEET 2

PRESSUk2(PSIG) 0.00 12.00 35.00 k5.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00 DATE 20/31 10/31 11/1 '11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 TIME 8.19 18.02 4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08 CAGE ' AZIMUTH 255 I . t 173R 0 -12 17 12 27 37 30 18 37 45 48 > 173R* O -28 -28 -27 -33 -35 -32 -37 -5 -8 -13

.(

p A21HU1H 165 I w - L g 174R .0 572 625 663 658 660 668 667 675 693 700 174 R* O -13 -17 -13 -23 -23 -15 -8 3 15 27

INDICATES REDUNDANT CACE n

f 4 i G

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             .                                                                                                                                I' 1ALLE 22                                                              ~

DOME LINLI. S1RAlh5 p.1CI G114./ In. ) t PFLESURE(PSIC) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00- 12.00 0.00 . LA7E 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 11t4E 8.19 18.02 4.04 11.48 19.11 2.41 9.25 14.35 19.58. 6.0C 12.08 [ .

               ' CAGE ii                 134tt            0     7      -3           7              27     37      37       37       7      -10          3 134D             0   -23     -00         -63            -E0    -80      -70      -50     -37      -23        -3 134I1            0    -7      40          73            127    163      137      11C . 93       13      -20 142tl             0     7       3          13             '33     40      40       47      23       13        10 142D              0   -10     -G3         -67            -63    -70      -50      -27     -33      -20          7

14211 0 -60 63 C7 107 230 160 123 220 47 -37 *

        .        13C6:             0    80     120         157            153    167      170      173      E7      100      213 138D              0    70      S7         120            107    22 7     227      317-    160      127      133 13Ett             0    23     137         177            240    260      250      21C     203       97        43 I

w 146tl 0 37 S7 117 137 167 153 140 57 53 to

       "         1460              0    20      23          33             37      40      53       67      47       50        50 14611             0   -37      C3         113            197    243      203      137     200       50      -50 151st             0    60     117         160            190    217      210      207     140      127      12C 1510              0    -7      03         117            110    210      107      143     173      '77        20 1511:             C    13     103         137            IS3    22 7     217      197     197      133-       SG

! 155t: 0 47 103 147 173 IS3 103 163- 100 63 53 1550 0 390 -183 -140 -63 50 63 33 1C 47 30 15511 0 -3 60 93 133 170 153 133 127 SC 10 t 15Eli 0 33 120 160 213 253 230 IS7 163 73 30 1550 0 -57 57 97 177 240 200 137 200 33 -63 ; 15511 0 43 120 100 207 240 21- 2C3 160 67 57 103t1 0 2913 -1766 -1357 -EL7 -C23 -820 -C47 -1470 -1C37 -1000 " 163D 0 183 -20L6 -2046 -1703 -1423 -1153 -1153 -1230 -150 -210 16311 0 37 113 150 217 200 337 323 2E0 467 487 L i, W V N s u;

                                                                                              . . a-  + ^uw anedurdwx,n
    , s ELEMSNT ORIENTATION r-OR MAX. SHEAR. STRESS                                                         !
                                                                                                /
                                                                                              /s
                                                                                         /      <M
                                                                                       /                                -
                                                                                     /

e% M ELEMENT ROTATED COUNTER. CLOCKWISE py T:4RU .C FOR MAX. & MIN. PRINCIPAL STRESS

                                                                             /         d             DIRECTICM
                                                                      > d A              /           %*
                                                                  /
                                                                /
                                               <          l gg. /                                      ROSEi i e ORIENTATION As A                 /                             PtJCED AND STRESSES IN dX p                        g               4           WE CR!GINAL.CRIENTATICN O    VTXY dY v

t ROS t=. : iE DATA OUTPUT KEY l l EIGURE .20 A-33

              %   $e,       -%qi-g-. p -u ,+w-                         a         m   >            -

-: . =- . :_ w. .. .~m+ auw:wiwwemw MAIN STEAM LINE PEHETRATION ROSETTE HUMBER 76 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIN./IN.> (PSI) (DEG)

MAX MIH SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 -59 -121 61 -3043 -4414 685 24.70 35.00 43. -147 190 -21 -4260 2119 34.19 45.00 121 -144 264 2465 -3432 2948 33.50 55.00 196 -106 302 5228 -1499 _3364 34.98 63.30 234 -110 344 6388 -1279 ~3834 35.08 55.00 211 -135 346 5447 -2272 3859 34.56 45.00 155 -162 317 3397 -3673 3535 33.88 35.90 120 -107 227 2808 -2256 2532 43.32 12.00 -37 -117 80 -2281 -4071 895 42.62 ~ 0.00 -47 -77 30 -2218 -2891 337 3.17 ROSETTE NUMBER 77 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIN./IH.> (PSI) (DEG) MAX MIH SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 8 -131 139 -1001 -4108 1553 34.48 35.00 180 -33 213 5418 657 2380 7.24 45.00 211 -38 249 6368 812 2778 7.76 55.00 294 16 277 9512 3330 3091 1.72 63.30 317 23 294 10321 3763 3279 1.95 55.00 294 -4 298 9332 2681 3326 2.89 45.03 237 -37 273 7191 1094 3048 6.34 35.00 386 84 302 13098 6371 3364 -10.02 12.00 134 -34 167 3936 206 1865 11.75 0.00 11 -141 152 -1000 -4386 1693 35.38 ROSETTE HUMBER 78 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIH./IN.)- (PSI) (DEG) MAX MIH SHEAR - MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00

                 .12.00                         3            -36          39          -257         -1124        434      29.52 35.00-                      18             -45          63             153       -1258        705     -35.78 45.00'                     54              -31          85          1431            -465      948     -24.09 55.00                    108               -24        132           3199               253  1473      -23.52 63.30                    136                 -6      -142           4278            1107    1585      -19.64 55.00                      81              -33        119           2229            -434    1331      -27.05
                 .45.00                      39              -66        105             623        -1728      1176      -35.78 35.00                      44           .-144         187              -16       -4158      2087       42.96 12.00                    -12               -78          65-       -1134          -2594       1730      37.63 0.00                       8            -41          49          -149         -1232        541     -37.03 A-34

a. .

             -            -            - - .                    :-        .       _ :_ a s                     a . a%:i    aANNNA MAIN STEAM LINE PEHETRATION ROSETTE HUMBER                          79 PRESSURE                                    STRAIHS                                   STRESSES                ANGLE
           ,       (PSIG)                            (MICROIN./1H.)                                      (PSI)                (DEG)

MAX MIH SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 U.00 12.00 1000 -960 1960 22688 -21031 21840 -44.81 35.00 669 -435 1104 17145 -7479 12312 42.58 45.00 '1002 -736 1738 24912 -13865 19389 42.80 55.00 676 -346 1021 18224 -4554 11389 39.64 63.30 680 -326 1006 18537 -3900 11218 38.49 55.00 365 -35 400 11300 2370 4465 28.62 45.00 672 -3?9 1062 17708 -5972 11840 40.76 35.00 679. -376 1055 18053 -5488 11770 38.71 12.00 669 -502 1171 16518 -9614 13066 42.39 0.00 667- -607 1273 15444 -12958 14201 45.00 - ROSETTE HUMBER 80 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIN./IN.> (PSI) (DEG) MAX HIH SHEAR MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 4 -61 65 -443 -1904 730 7.37 35.00 47 -20 67 1296 -191 744 0.00 45.00 ^60 -20 80 :724 -67 895 -2.38 55.00 77 23 55 2684 1458 613 -7.02 63.30 88 39 49 3165 2082 541 -7.97 55.'00 74 19 55 2546 1320 613 -7.02 45.00 57 -1< <3 1646 11 818 0.00 35.00 74 40 34 2727 1968 379 39.35 12.00 17 -10 27 445 -168 307 -7.02 0.00. -4 -69 66 -787 -2251 732 11.98 ROSETTE HUMBER 81 l PRESSURE STRAINS STRESSES ANGLE (PSIG) <MICROIN./IN.> (PSI) '(DEG) MAX HIH SHEAR MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 -3 -47 44 -540 -1532 496 -6.50 35.00 50 -0 51 1604 467 569 5.65 45.00 51 -178 229 -65 -5182 2558 27.23 55.00 84 -114 198 1587 -2830 2209

                                                                                                                             ^? lo 63.30                        71               29       43            2547                1595     476      1#.3^

55.00 54 16 38 1874 1026 424 i t, . N 45.00 27 . -3 30 820 1^7' 337 4i.A3 35.00 77 16 61 2619 124^ 6P'5 6.26

             ' 12.00                           24          -104         127            -236             -307c      14        23.56 0,00                    -33'           -101          68          -2003              -3520       7t.      39.35       l A-35                                                       1
 '..                                                                                                                                     \
                                   ...                -      .      = ..        _

_. w. . a .s_- _ m _ -m ~+c _ ushusen%wesutam MAIH STEAM LINE PEHETRATION ROSETTE HOMBER 82 3 PRESSURE STRAINS STRESSES ANGLE (PSIG) (NICROIH./IN.> (PSI) (DEG) MAX MIN SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 4 -7 11 49 -187 118 -35.78 35.00 136 -416 552 352 -11951 6151 22.74 45.00 97 -21 118 2906 269 1319 24.79 55.00 130 -20 151 3962 595 1683 21.61 63.30 144. -21 165 4398 711 1843 20.86 55.00 192 -425 617 2055 -11720 6887 22.72 45.00 95 -18 113 2851 325 1263 23.69 35.00 107 -20 127 3216 375 1420 23.56 12.00 67- -0 67 2128 634 747 2.86 0.00 29 -9 39 848 -19 434 -29.52 ROSETTE NUMBER 83 PRESSURE STRAINS STRESSES ANGLE (PSIG) (MICROIN./IN.> (PSI) (DEG) MAX MIN SHEAR MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 -333 -1000 667 -20181 -35051 7435 45.00 35.00 -333, -333 0 -13808 -13808 0 45.00 45.00 -0 -667 667 -6373 -21243 7435 45.00 55.00 -333 -1000 667 -20181 -35051 7435 0.00 63.30 -264 -736 471 -15455 -25970 5257 -22.50 55.00 -667 -667 0 -27616 -27616 0 45.00 45.00 -264 -736 471 -15455 -25970 5257 -22.50 35.00 -333 -333 0 -13808 -13808 0 45.00 12.00 -264 -736 471 -15455 -25970 5257 22.50 0.00 360 -694 1054 4852 -18660 11756 -35.78 ROSETTE HUMBER 84 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIH./IH.> (PSI) (DEG) MAX MIH SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 471 -471 943 10515 -10515 10515 22.50 35.00 138 -805 943 -3293 -24323 10515 22.50 45.00 -0 -667. 667 -6373 -21243 7435 0.00 55.00 540 -874 1414 8868 -22676 15772 22.50 63.30' -667 667 -6373 -21243 7435 45.00 55.00 -264 -736 471 -15455 -25970 5257 22.50

           -45.00                    360            -694       1054         4852 -18660                   11?56           9.22 35.00                  471            -471-       943        10515 -10515                   10515        22.50 12.00                     27        -1027        1054.      -8953 -32468                    11756        -9.22 0.00             .412            -1079        1491         2817 -30434                   16626        31.72 A-36
         ,                                 ~_

1. -

     ,.E .. ..
                                . , . , -        U..
                                                                                                                         '5..,  "# ,d      *
                                                                                                                                             ..c. *ab bli1d   dh N3M~d [

MAIN STEAM LIHE PEHETRATION ROSETTE HUMBER 85 PRESSURE- STRAIHS STRESSES ANGLE (PSIG) (MICROIN./IN.> (PSI) (DEG) MAX MIH SHEAR MAX MIH SHEAR 0.00 0 0 0 .0 0 0 0.00 12.00 333 -333. 667 7435 -7435 7435 45.00 35.00 69 -402 471 -1647 -12162 5257 22.50 45.00 333 -333 667 7435 -7435 7435 45.00 55.00 -0 -667 667 -6373 -21243 7435 45.00 63.30 360 -694 1054 4852 -18660 11756 -35.78 55.00 360- -694 1054 4852 -18660 11756 35.78 45.00 360 -694 1054 4852 -18660 11756 35.78 35.00 1016 ' -683 1700 25860 -12052 18956 39.35 12.00 360 -694 1054 4852 -18660 11756 35.78 0.00 360 -694 1054 4852 -18660 11756 -35.78 ROSETTE.HUMBER 86 PRESSURE STRAIHS STRESSES ANGLE (PSIG) <MICROIN./IH.) (PSI) (DEG) MAX MIH SHEAR MAX HIH SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 -264 -736 471 -15455 -25970 5257 22.50 35.00 -264 -736 471 -15455 -259?O 5257 -22.50 45.00 333 -1000 667 -20181 -35051 7435 45.00 55.00 -306 -1360 1054 -22764 -46276 11756 -35.78 63.30 -264 -736 471 -15455 -25970 5257 -22.50 55.'00 138 -805 943 -3293 -24323 10515 22.50 45.00 -333 -1000 667 -20181 -35051 7435 45.00 35.00 69 -402 471 -1647 -12162 5257 -22.50 12.00 -333 -1000 667 -20181 -35051 7435 45.00 0.00 -333 -1000 667 -20181 -35051 7435 45.00 ROSETTE HUMBER 87 PRESSURE STRAINS STRESSES ANGLE (PSIG) (MICROIN./IN.) (PSI) (DEG) MAX MIN SHEAR MAX MIH SHEAR

                     ^ 00                      0              0                    0                     0                  0           0                0.00 12.00                   323          ' 333 667               7435          -7435               7435              45.00 35.00                      69         -402                    471            -1647 -12162                         5257            -22.50 45.00                      69         -402                    471            -1647 -12162                         5257            -22.50 55.00                      69         -402                    471            -1647 -12162                         5257            -22.50 63.~30                     69         -402                    471           .-1647 -12162                         5257              22.50 55.00                             -667                    667            -6373 -21243                         7435              45.00 45.00-                     69         -402                    471            -1647 -12162                         5257            -22.50 35.00                     -0          -667                    667            -6373 -21243                         7435                 0.00 12.00                     69          -402                    471            -1647 -12162                         5257              22.50 0.00                    -0          -667                    667            -6373.-21243                         7435              45.00 A-37'

1

  .. . -: :.--.~              w._ t                =     .

x_ - _=.: :a a - w:ewiemuca.:..y l MAIH STEAM lit 1E pet 1ETRATI0t1 ROSETTE'HUMBER 88 - s- __________________ PP, ESSURE' STRAIHS STRESSES ANGLE (PSIG) (MICR0IH./IN.) - (PSI) (DEG) MAX MIN SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 -0 -667 667 -6373 -21243 7435 45.00 35.00 333 -333 667 7435 -7435 7435 45.00 45.00 360 -694 1054 4852 -18660 11756 35.78 55.00 -333 -333- 0 -13808 -13808 0 45.00 63.30 -0 -667 667 -6373 -21243 7435 45.00 55.00 -264 -736 471 -15455 -25970 5257 -22.50 45.00 69 -402 471 -1647 -12162 5257 22.50 35.00 333 -333 667 7435 -7455 7435 45.00 12.00 -333 -333 0 -13808 -13808 0 45.00 0.00 -264 -736 471 -15455 -25970 5257 -22.50 . ROSETTE HUMBER 89 PRESSURE STRAIHS STRESSES . RHGLE (PSIG) (MICROIH./IN.) (PSI) (DEG) MAX MIH SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 -333 -333- 0 -13808 -13808 0 45.00 35.00 69 -402 471 -1647 -12162 5257 22.50 45.00- -0 -667 667 -6373 -21243 7435 0.00 55.00 360 -694 1054 4852 -18660 11756 35.78 63.30 69 -402 471 -1647 -12162 5257 22.50 55.00 360 -694 1054 4852 -18660 11756 35.78 45.00 -264 -736 471 -15455 -25970 5257 -22.50-35.00 -0 -667 667 -6373 -21243 7435 0.00 12.00 -264 -736 471 -15455 -25970 5257 -22.50 0.00 -667 -667 0 -27616 -27616 0 45.00 A-38

      ,-              . a..       .: = :a =                . :.x mw                  :aq   w awm=u ams. .       '

FEEDWATER LINE PEHETRATION ROSETTE HUMBER 90 7 , PRESSURE STRAINS STRESSES ANGLE (PSIG) (MICROIN./IN.) (PSI) (DEG) MAX MIH SHEAR MAX MIN SHEAR 0.00 0 0 0 'O O O 0.00 12.00 138 -805 943 -3293 -24323 10515 22.50 35.00 333 -1000 1333 1062 -28678 14870 45.00 45.00 138 -805" 943 -3293 -24323 10515 22.50 55.00 412 -1079 1491 2817 -30434 16626 31.72 63.30 27 -1027 1054 -8956 -32468 11756 9.22 55.00 -0 -1333 1333 -12746 -42487 14870 0.00 45.00 27 -1027 1054 -8956 -32468 11756 9.22 35.00 138 -805 943 -3293 -24323 10515 22.50 12.00 138 -805 943 -3293 -24323 10515 22.50 0.00 -195 -1138 943 -17101 -38131 10515 22.50 . ROSETTE HUMBER 91 PRESSURE STRAIHS . STRESSES ANGLE (PSIG) (MICR0lH./IN.> (PSI) (DEG) MAX MIH SHEAR MAX HIH SHEAR. 0.00 0 0 0 0 0 0 0.00 12.00 333 -1000 1333 1062 -28678 14870 45.00 35.00 138 -805 943 -3293 -24323 10515 22.50 45.00 79 -1412 1491 -10991 -44242 16626 31.72 55.00 -0 -667 667 -6373 -21243 7435 0.00 63.30 -0 -667 667 -6373 -21243 7435 0.00 55.00 540 -874 1414 8868 -22676 15772 22.50 45.00 69 -402 471 -1647 -12162 5257 22.50 35.00 360 -694 1054 4852 -18660 11756 35.78 12.00 69 -402 471 -1647 -12162 5257 22.50

            .0.00               -0           -667      667        -6373 -21243               7435         0.00 ROSETTE HUMBER                  92 PRESSURE                             STRAIHS                             STRESSES              ANGLE (PSIG)                    (MICROIH./IH.)                                (PSI)               (DEG)

MAX MIN SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 360 -694 1054 4852 -18660 11756 -35.78 35.00 -333 -1000 667 -20181 -35051 7435 45.00

         -45.00.           -667             - -667       0       -27616 -27616                  0      45.00 55.00            -598            -1069-      471       -29263 -39773               5257      22.50    ,

63.30 -333 -1000 667 -20181 -35051 7435 0.00 55.00

         ~4 5.00           -oor              -ee7'      .0       -27616 -27616                  0      45.00 s          35.00--            '-0            '667 667        -6373 -21243               7435      45.00 12.00              138             -805      943        -3293 -24323- 10515                 -22.50 0.00           -333: -1000                 667       -20181 -35051               7435      45.00 A-39

       .a :- =              w .= w                ,.w   '       '
                                                                       + n : : u.uxwwwam.rmv FEEDWATER LINE PENETRATION 3      ROSETTE HUMBER             94 STRESSES                 ANGLE PRESSURE                      STRAIHS (PSI)                    (DEG)

(PSIG) (MICROIH./IH.) SHEAR MAX MIH SHEAR MAX MIN 0 0 0 0 0.00 0.00 0 0 294 6057 -24.24 12.00 425 -118 543 12409

                                         -393         496              -470 -11543           5536       -20.32 35.00            103
                                                                       -613 -11400           5394       -19.42
            .45.00             '97       -387         484 77                     77              2450           726      862           3.72 55.00                            -0 1086 -11166           6126       -19.79 63.30            153        -396         549
                                          -395        530                527 -11297          5912       -19.95 55.00           135
                                                                       -445 -11430           5493       -19.75 45.00           103         -390        492 3W              36      354             12783        4891      3946       -23.65 35.00                                                                          5323       -20.52 12.00             85        -392        477            -1029 -11675
                                          -779        859            -4921 -24076            9578       -21.24 0.00            79                                                                                       .

ROSETTE HUMBER 95 STRESSES ANGLE PRESSURE STRAIHS (PSI) (DEG) (PSIG) (MICR0lH./IN.> MAX HIH SHEAR MAX -MIN SHEAR 0 0 0 0 0.00 0.00 0 0

                                                                                  -1348         105        22.50 12.00            -25           -35           9          -1138
                                             -27       123              2826            74    1376         44.23 35.00              97 319     1338         45.00 45.00            100           -20       120              2995
                                               -7      143              4292         1094     1599       -44.33 55.00            137 1996     1525       -44.30 63.30            153             17      137              5046 0     140              4461         1338     1561         45.00 55.00            140 297    1636          45.00 45.00            120           -27       147              3569 20      147              5504         2229     1637          43.70 35.00             167
                                                                                     -927     1825          43.25 12.00            103          -60       164              2723
                                           -103        13<                 <5     -2975       1525          44.30 0.00             33 ROSETTE HUMBER             96 STRESSES                   ANGLE PRESSURE                      STRAIHS (PSI)                     (DEG)

(PSIG) (MICROIN./IH.) MAX MIH SHEAR MAX MIH SHEAR 0- 0 0 0 0 0.00 0.00 0 5257 22.50 12.00 69 -402 471 -1647 -12162

                             -264          -736        471           -15455 -25970            5257       -22.50 35.00                                                                          5257       -22.50 45.00         -264          -736        471           -15455 -25970-
                             -264           -736       471           -15455 -25970            5257           22.50 55.00                                                                         11756           35.78 63.30         -306        -1360        1054           -22764 -46276
                             -333        -1000         667           -20181 -35051            7435           45.00 55.00                                                                                         45.00 a'  '
              -45.00         -667           -667            0        -27616 -27616                    0
                              -195 --1138              943           -17101 -38131 10515                     22.50 35.00                                                                                         22.50 12.00         -195- -1138              943           -17101 -38131 10515 0.00         -333        -1000        667           -20181 -35051             7435          45.00 s

A-40

- .-   x--             /             _~       -
                                                     .       wa         .ww.aw ws axmmrea FEEDWATER LINE PEHETRATION
     ^ ROSETTE-HUMBER         98 STRESSES                  ANGLE STRAIHS                                                            (DEG)

PRESSURE (MICR0!N./IH.> (PSI) (PSIG) SHEAR MAX MIN SHEAR MAX MIN ______-_____-_-____ _____ ________ _____._____________ O 0.00 0 'O O 0.00 0 0 5257 -22.50

                    -264           -736           471           -15455 -25970 12.00                                    943             -3293 -24323          10515       -22.50 35.00        138          -805                                                 10515       -22.50 138          -805           943             -3293 -24323                           0.00 45.00                                    667             -6373 -21243           7435 55.00-          -0        -667                                                 10515       -22.50 138         -805           943             -3293 -24323                         22.50 63.30                                   943             -3293 -24323          10515 55.00        138         -805                                                 10515          22.50
                     -195 -1138                   943            -17101 -38131                      -22.50 45.00                                   471             -1647 -12162           5257 35.00.         69         -402                                                  5257       -22.50
                     -264           -736          471            -15455 -25970                           0.00 12.00                                   667            -20181 -35051            7435 0.00     -333         -1000                                                                           .

ROSETTE HUMBER 99 STRESSES ANGLE PRESSURE -STRAINS (DEG) (PSI) (PSIG) (MICROIN./IN.> MIN SHERR NAX MIH SHEAR MAX .____ 0 0 0 0.00 0.00 0 0 0 -22.50 913 10515 -10515 10515 12.00 471- -471 10515 -22.50 138 -805 943 -3293 -24323 -22.50 35.00 943 -3293 -24323 10515 45.00 138 -805 10515 -22.50 138 -805 943 -3293 -24323 -22.50 55.00 943 -3293 -24323 10515 63.30 138 -805 10515 -22.50 138 -805 943 -3293 -24323 -22.50 55.00 943 -3293 -24323 10515 45.00 138 -805 16626 -13.28 412 -1079 1491 2817 -30434 -22.50 35.00 943 -3293 -24323 10515 12.00 138 -805 10515 -22.50 0.00 138 -805 943 -3293 -24323 ROSETTE HUMBER 100 STRESSES ANGLE STRAIHS - (DEG)

         . PRESSURE (MICROIH./IN.>                                (PSI)

(PSIG) SHEAR MAX MIN SHERR MAX MIH ___________________ _____ ________ ___________________ 0.00

                                                                          'O          O           O 0             0            0                                             -31.72 0.00                                                  16626 -16626         16626 12.C0        745          -745         1491 11756        -35.78
                                       -360         1054             18660 -4852 35.00        694 22305 -22305         22305           45.00 45.00      1000         -1000          2000                                                  35.78 4852 -18660         11756 55.00-        360         -694         1054 10515          22.50 471         -471           943            10515 -10515 63.30                                    471            12162       1647       5257           22.50 55.00        -402           -69                                               16626           31.72 745         -745         1491              16626 -16626                         45.00

' 45.00 14870 -14870 14870 35.00 667 -667 1333 7435 0.00

                             -0         -667           667           -6373 -21243                          22.50 12.00                                    471           -1647 -12162            5257 0.00          69         -402 A-41

            . :. . :-            =                           --
                                                                                                     .- a a -        mmm

k. '

L FEEDWATER LIHE PENETRATION ROSETTE HUMBER 101

s. __________________

PRESSURE STRAIHS STRESSES ANGLE (PSIG) -(NICROIN./IN.> (PSI) (DEG) MAX HIH SHEAR MAX MIH SHEAR 0.00 0 0 0 :0 0 0 0.00 12.00 360 -694 1054 4852 -18660 11756 -35.78 35.00 27 -1027 1054 -8956 -32468 11756 -35.78 45.00 -264 -736 471 -15455 -25970 5257 22.50 55.00 -0 -667 667 -6373 -21243 7435 45.00 63.30 -264 -736 471 -15455 -25970 5257 22.50 55.00 -0 -667 667 -6373 -21243 7435 45.00 45.00 -0 -667 667 -6373 -21243 7435 45.00 35.00 360 -694 1054 4852 -18660 11756 35.78 12.00 360 -694 1054 4852~-18660 11756 -35.78

                     ~0.00           360              -694      1054            4852 -18660                 11756    -35.78    .

ROSETTE HUMBER 102 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIH./IN.> (PSI) (DEG) MAX HIH SHEAR MAX HIH SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 724 -667 1391 16689 -14341 15515 43.83 35.00 387 -697 1084 5666 -18507 12086 35.39 45.00 975 -689 1664 24495 -12620 18558 -38.40 55.00 633 -667 1300 13813 -15194 14503 -44.27 63.30 735 -352 1087 20069 -4190 12129 -37.45 55.00 1404 -717 2121 37877 -9432 23655 -36.12 45.00 667 -667 1333 14870 -14870 14870 45.00 35.00 710 -357 1067 19219 -4582 11900 -36.46 12.00 660 -667 1327 14658 -14934 14796 -44.86 0.00 630 -667 1297 13708 -15227 1446?. -44.19

(,

A-42 a r

__ ..C_a - c_ u ,:2 .- a m > > wmwa: SPARE PEHETRATION ROSETTE HUMBER 104 PR2S3URE- STRAIHS STRESSES ANGLE (PSIG) (MICROIN./IN.) (PSI) (DEG) MAX MIH SHEAR MAX MIH RHEAR 0.00 0 0 0 'O O 0 0.00 12.00 -333 -333 0 -13308 -13808 0 45.00 35.00 -333 -333 0 -13808 -13808 0 45.00 45.00 138 -805 943 -3293 -24323 10515 -22.50 55.00 69 -402 471 -1647 -12162 5257 -22.50 63.30- 69 -402 471 -1647 -12162 5257 22.50 55.00 -0 -667 667 -6373 -21243 7435 45.00 45.00 -333 -333 -0 -13808 -13808 0 45.00 35.00 -264 -736 471 -15455 -25970 5257 22.50 12.00 -264 -736 471 -15455 -25970 5257 22.50 0.00 -667 -667 0 -27616 -27616 0 45.00 . ROSETTE HUMBER 105 PRESSURE STRAINS STRESSES ANGLE (PSIG) (MICROIN./IN.> (PSI) (DEG) MAX MIH SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 T. 12.00 360 -694 1054 4852 -18660 11756 -35.78 35.00 -0 -667 667 -6373 -21243 7435 45.00 45.00 69 -402 471 -1647 -12162 5257 -22.50 55.00 -0 -667 667 -6373 -21243 7435 45.00 63.30 360 -694 1054 4852 -18660 11756 35.78 55.00 764 -736 471 -15455 -25970 5257 22.50 45.00 683 -1016 1700 12052 -25860 18956 39.35 35.00 360 -694 1054 4852 -18660 11756 35.78 12.00 333 -1000 1323 1062 -28678 14870 45.00 0.00 27 -1627 1054 -8956 -32468 11756 35.78

             - ROSETTE HUMBER 108 PRESSURE                             STRAINS                                  STRESSES               ANGLE (PSIG)                    (MICROIH./IN.)                                     (PSI)               (DEG)

MAX MIH -SHEAR MAX MIN SHEAR 0.00 0. 0 0 0 0 0 0.00 12.00 41. --31 71 1003 -588 796 -18.70 35.00 80 126 54 2509 1610 599 -14.87 45.00 97 :50 47 3564 2512 526 -4.07 55.00 117 69- 48 4402 3330 536 -16.85 63.30 115 95 .19 4566 4'133 217 -15.48 55.00 117 73 43 4420 3451 485 -28.76 g/ z 45.00 122 33 84 4246 2382 932 -30.69 35.00.: 85 65 19- 3324 2890 217 15.48 12.00 77 -4 81 2423 614 905 -40.27 0.00' 75 -52 127 1899 -932 1416 -33.40 A-43

         .~ . .e   ..n               an A                        -

a. :- - - wa woua awr ,mww SPARE PEtlETRATIGN ROSETTE HUMBER 109 y __________________

PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIN./IH.) (PSI) (DEG) MAX MIN SHEAR MAX MIH SHEAR ________ _______m___________ ___________________ _____ 0.00 0 0 0 0 0 0 0.00 12.00 37 -123 160 -9 -3581 1786 43.81 35.00 87 -63 150 2157 -1190 1673 -44.36 45.00 103 -53 157 2783 -712 1748 -44.39 55.00 104 -0 104 3298 982 1158 -42.24 63.30 111 35 76 3886 2190 848 -37.37 55.00 107 10 97 3500 1333 1034 -42.05 45.00 100 -27 127 2934 104 1415 -43.49 35.00 90 63 27 3482 2869 307 37.98 12.00 45 -18 63 1258 -153 705 35.78 0.00 39 -129 167 3 -3731 1867 38.67 . ROSETTE HUMBER 110 PRESSURE STRRIHS STRESSES ANGLE ' (PSIG) (MICROIN./IN.> (PSI) (DEG) MAX MIN SHERR MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00 J 12.00 -50 -240 191 -3879 -8134 2127 42.49

35.00 -3 -100 97 -1056 -3224 1084 33.92 45.00 7 -84 92 -567 -2609 1021 28.44 55.00 57 -7 63 1743 328 707 1.51 63.30 133 34 99- 4557 2347 1105 -23.86

                   -55.00                   70                  13       58        2368                 1084   642        -5.00 45.00-                 29               -52         81            417          -1383      900        25.85 35.00                196                   74      122        6956                 4228  1364       -36.28 12.00                  21               -54         75            141          -1522      831        39.85 0.00              -43              -290          247       -4149              -9659    2755        43.45 ROSETTE HUMBER 111 PRESSURE                                STRAIHS                                 STRESSES                ANGLE (PSIG)                       (MICROIH./IN.>                                     (PSI)                (DEG)

MAX MIH SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 .-16 -130 114 -1767 -4308 1271 34.72 35.00 28 9 '5 904 338 283 11.60 45.00 40 -0 41 1281 376 452 4.73

                   '55.00                   93                  27       66        3222                 1749   736       -22.50 63.30               155                    41      114        5345                 2802  1272       -37.37 55.00                -95                   28       67-       3307                 1802   753       -28.55          l 45.00-                 44                     2     42         1437                 496   470           9.22        l
     ~               35.00              -134.                   46       89        4720                 2736   992        38.50        .i 12.00                  27               -43         70           436           -1127      782       -43.64          l
                    'O.00                   -3            -230          227       -2301             -7365     2532        43.32          i
                                                            ?              -A-44                                                 -

l b - _ j

       .c~._c a s s a u                   .._.a.                    --m.w a n ww                             agemw SPARE PEHETRATION ROSETTE HUMBER 112 PRESSURE                            STRAIHS                              STRESSES                  ANGLE (PSIG)                  (MICROIH. / Ill. )                             (PSI)                   (DEG)

MAX MIN SHEAF. MAX HIH SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 -33 -114 81 -2139 -3906 898 32.78 35.00 45 -18 63 1254 -149 701 -29.00

                ~45.00                 91            -15      106           2769                406    1181      -32.93 55.00              188                -5    192           5943              1652     2145   .
                                                                                                                 -40.51 63.30             245                  5    239           7849             2507      2671      -40.60 55.00               198                -4    202          6255               1754     2250      -41.20 45.00               134             -14      147          4128                 843    1642      -42.40 35.00              237                 27    210          7799              3109      2345       43.64 12.00               44            -10       54           1290                  91    599       30.13 0.00           -36            -107        71        -2173             -3764        796      -26.30 CSETTE HUMBER 113                                    .

PRESSURE STRAINS STRESSES ANGLE (PSIG) (MICROIN./IN.> (PSI) (DEG) MAX MIN SHEAR MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00 , 12.00 67 -113 180 1042 -2975 2009 -43.94 ( 35.00 186 -103 289 4949 -1497 3223 '-39.35 45.00 253 -140 394 6737 -2042 4389 -39.63 55.00 264 -97 361 7476 -572 4024 -36.95 63.30 281 -65 346 8347 628 3859 -34.56 55.00 275 -92 36r <889 -294 4092 -36.28 45.00 239 -109 348 6579 -1194 3887 -37.52 S3.00 169 14 154 5519 2075 1722 -28.67 12.00 91 -61 153 2327 -1085 1706 -39.35 0.00 53 -140 193 362 -3953 2157 44.01 ROSETTE HUMBER 114 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIN./IN.) (PSI) (DEG) MAX MIN SHEAR MAX MIN SHEAR 0.00" 0 0 0 0 0 0 0.00 12.00 79 -146 225 1127 -3889 2508 -39.01 35.00 152 -82 235 4066 -1167 2617 -33.72 45.00 194 -94 287 5274 -1132 3203 -34,10 55.00- 217 -47 264 6464 578 2943 -31.88 63.30 235 -18 253 7306 1670 2818 -29.52 55.00 .213- -43 255 6366 676 2845 -30.55 45.00 182- ~72 255 5122 -565 2843 -32.22 35.00 127- '57 70 4579 3016 782 1.36 12.00 51 105 .1098 -1236 1167 .M.L3 0.00 16 -163 179 -1036 -5040 2002 -3x.10 A-45

        /!
 , .. e <           w.    . 2  ____.m A2                      ..            ..n  .ssg
                                                                                                       %.mm ., <mmwwa,vs SPARE PEHETRATION ROSETTE liUMBER.115 x       __________________

PRESSURE STRAINS STRESSES A!CLE (PSIG) ,MICROIH./IH.) (PSI) (DEG) MAX f4 :H SHEAR MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00 12.00- 3 -47 50 -339 -1456 559 -43.09 35.00 91 6 85 2950 1054 948 -32.22 45.00: 118 8 110 3854 1393 1231 -32.49 55.00. -164 30 134 5501 2508 1496 -31.72 63.30 210 33 178 7022 3058 1982 -33.49 55.00 183 31' 152 6117 2720 1699 -33.40. 45.00 140 20 120- 4654 1974 1340 -35.28

                ~35.00-               147                76            71         5421              3830         796      -26.30 12.00                41               26            15          1547              1215         166     -31.72 0.00               -9            -34              25         -614            -1181          283        11.60   .

ROSETTE ~HUMBER 116 PRESSURE STR' Ills . STRESSES ANGLE (PSIG) (MICRO.1./IN.) (PSI) (DEG) MAX MIN SHEAR MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00 t 12.00 7- -117 125 -886 -3670 1392 17.06 35.00 72 -35 108 1959 -441 1200 -8.09 45.00 96 -46 141 _614 -542 1578 -7.51 55.00- 145 -8 153 4533 1128 1703 -18.06 63.30 185 9 176 5967 2041 1963 -26.35 55.00: 147 -4 151 4659~ '1279 1690 -19.82 45.00 111 -28 139 3279 173 1553 -10.52 35.00 170 43 127 5839 2998 1420 -42.00 12.00 43 -20 63 1191 -224 707 1.51

0.00 13: L-157 170 -1075 -4862 1893 23.30 ROSETTE HUMBER 117

             . PRESSURE                            STRAIHS                                    STRESSES                     ANGLE (PSIG)                    (MICROIN./IH.>                                       (PSI)                     (DEG)

MAX MIN SHEAR MAX MIH SHEAR 0.00 0 0 0 0 .0 0 0.00 12.00 17 85 -88 -1983 948 -24.09 35.00 ~120 -16 136 3654 627 1514 -32.66 45.001 157- -27 184 4743 642 2050 -33.81 55.00 198 2 .196 6329 1956 2187 -36.09 63.30- 245 11 234. 7926 2706 2610 -39.67 55.00' 223 -10 233 7016- 1822 2597 -38.38 45.00 204 -37 241 6139 765 2687 -37.79

      '           35.00              207-             '30           177          6873- 2931                    1971        44.46
                ~12.00:              114             -48            162          3190              -428        1809      -40.27
                  -0.00                60          -120             179-            759 -3245-                2002       -37.47 A-46
  , ,      ~

a . . . =.-+ . ; . :_ :u w-w ,.s.a.:wuw 3 : ~ -a - , ~~ LIHER GAGES ROSETTE HUMBER 70 s __________________ PRESSURE STRA'.L STRESSES ANGLE (PSIG) (MICROIH./IN.) (PSI) (DEG) MAX MIN SHEAR MAX MIN SHEAR 0.6? O O O O O O 0.00 12.00 -26 -141 115 -2169- -4736 1284 -5.00 35.00 -10 -74 64 -1011 -2441 715 -4.49 45.00 -3 -87 35 -916 -2812 949 -5.65 55.00 30 -7 37 894 73 411 -2.60 63.30 52 28 24 1925 1389 268 16.85 55.00 13 0 -23 53 733 -457 595 0.00 45.00 7 -70 77 -456 -2168 856 -1.24 35.00 89' 37 52 3204 2043 581 -19.90

                -12.00              -31              -65       34           -1619             -2385         383     14.53 O.00             -89            -174        85           -4506             -6402         948   -12.78         .

ROSETTE HUMBER 71 PRESSURE . STRAINS STRESSES ANGLE (PSIG) (NICROIN./IN.) (PSI) (DEG) MAX MIH SHEAR , MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00

 -('             12.00             - 405             -75     481             12198               1472      5363   -22.78 35.00              777              -77     854            24026               4971       9528   -21.08 45.00              386              -10     396             1E221              3383       4419   -21.48 55.00               166           -429      594                1175 -12084                6630   -23.64 63.30              249            -836     1084                  24247              12096   -23.25 55.00              296         -1226       1523            -2280 -36244                  16982   -22.68 45.00              o'15        -2010       2432            -60F0 -60337                  27129   -22.33 35.00              363         -1616       1980            -3877 -48042                  22082   -22.23 12.00              496         -2799       3295           -10954 -84460                  36753   -22.09 0.00             530         -3190       3720           -13608 -96581                  41487   -22.03 ROSETTE HUMBER                  72 PRESSURE                             STRAIHS                                 STRESSES                ANGLE (PSIG)                     (MICROIN./IH.)                                   .(PSI)                (DEG)

MAX MIN SHEAR MAX MIH SHEAR 4 l 0.00 0 0 0 0 0 0 0.00 J 12.00 "4 -49 45 -606 -1603 499 31.72 35.00 35 1 34 1142 377 383 -30.47 45.00 56 7 49 1861 763 549 -30.85 55.00 102 35 67 3583 2078 753 -16.45 63.30 118 39 78 4120 2370 875 -6.13 H55.00- 88 32 57 3121 -1850 635 -10.28

               '45.00                 57                23     33             2029               1285       372   -26.57
   --           35.00                 83                44     E              M57               2190       ~434    15.48 12.00                 18               -8     25                490               -76      283    11.60 0.00               -5             -52       47             -645            -1702         528    19.64           l I

A-47. i

   ._        :.u .m   ,.    ...m.__.._           .         m.          c.a    -2                 .m e -     %       e m"+.u LINER GAGES ROSETTE tlUMBER               73 PRESSURE                           STRAINS                            STRESSES             ANGLE (PSIG)                  (MICR0!H./IN.)                               (PSI)             (DEG)

MAX MIN SHEAR MAX MIN SHEAR 0.00- 0 0 0 0 0 0 0.00 12.00 38 -62 100 631 -1597 1114 -12.85 s 35.00 104 -8 112 3252 752 1250 -11.38 45.00 136 0 136 4344 1317 1514 -12.34 55.00 179 48 131 6156 3234 1461 -7.37 63.30 197 53 144 6787 3569 1609 -3.32 55.00 183 46 137 6292 3236 1528 -9.22 45.00 170 40 130 5804 2895 1454 -16.24 35.00 134 96 38 5188 4340 424 7.63 12.00 95 12 82 3129 1290 920 -37.98 0.00 69 -52 120 1689 -998 1343 -37.79 . ROSETTE HUMBER 74 PRESSURE STRAINS . STRESSES ANGLE (PSIG) (NICROIH./IN.) (PSI) (DEG) MAX MIH SHEAR MAX MIN SHEAP, 0.00 0 0 0 0 0 0 0.00 12.00 47 -84 131 702 -2221 1462 -41.35 35.00 103 -10 113 1197 669 1264 -30.96 45.00 145 8 137 4707 1645 1531 -30.47 55.00 197 70 127 6944 4103 1420 -21.44 63.30 218 89 129 7795 4908 1444 -17.25 55.00 201 63 138 6993 3915 1539 -26.43 45.00 196 44 152 6670 3272 1699 -33.40 35.00 185 138 47 7225 6169 528 19.64 12.00 94 -1 95 2998 869 1065 38.95 0.00 65 -118 183 937 -3146 2042 39.75 ROSETTE HUMBER ~75 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICR0!H./IN.) (PSI) (DEG) MAX HIH SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 -59 -97 38 -2821 -3669 424 26.06 35.00 -58 -179 120 -3558 -6245 1343 37.79 45.00 -59 -187 128 -3679 -6539 1430 40.51 55.00 -4 -213 209 -2152 -6823 2335 38.09 63.30 20 -200 221 -1264 -6192 2464 42.40 55.00 37- -233 270 -1062 -7085 3011 44.65

   '('                    45.00              44          -284      328        -1316            -8626     3655    42.67 e'                 35.00            186           -319      504           2864          -8387     5626    41.20 12.00            104           -271      375             728         -7632     4180    42.45 0.00             67          -203      270             181         -5842     3011   -44.65 A-48 x

        -         .~.          -   _-                        u.               a w . u.                        m e x c :.mwou w LIllER GAGES ROSETTE ilUf18ER 134 PRESSURE                                'STRAIHS                              STRESSES                   At1GLE (PSIG)                        (MICR0Ill. /IN. >                              (PSI)                    (DEG)

MAX MIH SHEAR MAX HIH SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 24 -24 49 541 -541 541 37.03 35.00 119 -82 201 3005 -1487 2246 -33.79 45.00 168 -88 255 4507 -1193 2850 -37.44 55.00 241 -88 329 6844 -492 3668 -36.15 63.30 291 -91 382 8399 -114 4256 -35.31 55.00 251 329 7258 -78 3668 -36.15 45.00 202 -55 257 5908 168 2870 -36.72 35.00 147 -47 194 4233 -90 2161 -31.72 12.00 29 -26 55 684 -546 615 -32.49 0.00- 4 -21 25 -62 -628 283 -11.60 . ROSETTE HUMBER 142

PRESSURE STRAIHS STRESSES At1GLE (PSIG) (MICROIN. /Itl. ) (PSI) (DEG) MAX MIN SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 11 -64 75 -273 -1936 831 -13.28 35.00 135 -68 202 3638 -877 2258 -36.38 45.00 172 -72 245 4799 -657 2728 -36.28 55.00 300 -80 379 8784 329 4228 -33.07 63.30 361 -91 452 10632 553 5040 -32.57 55.00 285 -65 349 8452 661 3895 -33.19 45.00 203 -33 236 6155 888 2633 -35.53 35.00 305 -62 367 9134 946 4094 -28.30 12.00 83 -23 105 2418 67 1176 -35.78 0.00 17 -44 61 133 -1238 685 -20.30 ROSETTE HUMBER 138 PRESSURE STRAIHS STRESSES At1GLE (PSIG) (MICROIN./IN.> ' (PSI) (DEG) MAX HIH SHEAR MAX MIH SHEAR 0.00 0 0 0 0 0 0 0.00 I 12.00 85 18 67 2893 1388 753 -16.45 1 35.00 161 96 65' 6047 4586 730 -37.63 l 45.00 -214 119 95 7969 5840 1065 -38.95 l 55.00 241 152 89 9139 7155 992 -6.50 ' 63.30 280 167 114 10518 7985 1266 1.68

           -55.00                   253                167       87          9666             7733       967-        11.31 45.00                 318                  65     253-        10758             5122      2818         40.83 v         35.00                 205                  85     120          7350             4663      1343            7.21 12.00                 127                 70      57          4706             3440       633        -43.32
               .0.00                213                  43     170          7215             3417      1899         -1.68 A-49                                                         ,

1 l i l

 - -   . _          z..w .
                                         - ; , - .a .
                                                                ._w    . +E                         x .nnwm:s"we LINER GAGES ROSETTE HUMBER 146 PRESSURE                         STRAIHS                                      STRESSES            ANGLE (PSIG)                  (MICR0!H./IH.>                                        (PSI)             (DEG)

MAX MIN SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00 42 -42 84 , 932 -932 932 -14.31 35.00 157 23 134 5223 2234 1494 42.14 45.00 197 33 163 6586 2942 1822 44.42 55.00 300 33 267' 9880 3928 2976 -38.50 63.30 374 36 339 12270 4714 3778 -38.46 55.00 306 51 255 10231 4544 2843 -39.35 45.00 210 67 143 7329 4131 1599 44.33 35.00 262 34 228 8688 3601 2544 -31.53 12.00 54 49 5 2193 2088 53 22.50 0.00 71 -71 141 1577 -1577 1577 -22.50 . ROSETTE HUMBER 151 PRESSURE STRAIHS STRESSES ANGLE (PSIG)- (MICROIH./IN.> (PSI) (DEG) MAX MIN SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 . 0 0.00 (. 12.00 86 -13 98 2617 421 1098 30.85 35.00 137 83 55 5170 3944 613 37.98 45.00 182 115 67 6897 5392 753 34.89 55.00 213 170 43 8424 7455 485 -42.80 63.30 234 209 25 9466 8899 283 -33.40 55.00 240 186 54 9437 8238 599 -41.44 45.00 260 143 117 9660 7048 1306 42.55 35.00 197 140 58 7615 6331 642 5.00 12.00 183 77 107 6577 4193 1192 -43.21 0.00 191 19 173 6275 2424 1925 40.00 ROSETTE HUMBER'155 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIH./IN.> (PSI) (DEG) MAX MIH SHERR MAX MIN SHEAR 0.00 0- 0 0 0 0 0 0.00 12.00 391 -347 738 9132 -7337 8235 -43.06 35.00 348 -184 532 9314 -2548 5931 42.66 45.00 331 -141 523 10801 -859 5830 42.07 55.00 371 -64 435 11205 1498 4853 42.36 63.30 314 49 264 10474 4577 2948 42.47 '

          .55.00             274                62          212           9339             4607   2366     40.93 45.00             264                32          232           8731             3558   2587     41.28 v          35.00             218                 9          208           7019             2371   2324    -41.32 12.00=              69              45            24          2615             2079    268     28.15 0.00              53              10            43          1796                827  435        2.20 A-50

_;.. .u - a. ..2_ w. ; w- _m .. _.. <m ..sumuzwwwm . LIHER GAGES ROSETTENdMBER'159 PRESSURE' STRAIHS STRESSES ANGLE (PSIG) (MICR0Ill. /IH. ) (PSI) (DEG) MAX MIN SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 12.00- 133 -57 190 3710 -534 2122 -43.49 35.00 183 57 127 6384 3558 1413 45.00 45.00 223 97 127 8041 5215 1413 45.00 55.00 243 176 67 9446 7952 747 42.14 63.30 256 237 19 10428 10008 210 22.50 55.00 254 200 54 9989 8790 599 41.44 45.00 263 137 127 9700 6870 1415 -43.49 35.00 200 123 77 7553 5841 856 ~ -43.76 12.00 127 33 94 4365 2262 1051 -40.93 0.00 151 -64 215 4193 -603 2398 -41.44 . ROSETTE NUMBER 163 PRESSURE STRAIHS STRESSES ANGLE (PSIG) (MICROIN./IN.) (PSI) (DEG) MAX MIN SHEAR MAX MIN SHEAR 0.00 0 0 0 0 0 0 0.00 ( 12.00 3408 -458 3866 104222 17980 43121 20.96 35.00 745 -2398 3144 820 -69308 35064 -26.64 45.00 id25 -2231 3256 11323 -61308 36316 -31.22 55.00 1164 -1804 2967 19841 -46352 33096 -34.40 63.30. 1005 -1548 2554 17230 -3970. 29484 -32.20 55.00 838 -1321 2159 14071 -34092 24i;2 -28.80 45.00 838 -1362 2200 13699 -35378 24538 -28.94 35.00 486- -1676 2162 -532 -48763 24115 -17.98 12.00 473 -1043 1515 5094 -28706 16900 3.60 0.00 488 -1001 1489 5981 -27245 16613 1.80 l

.~

A-51 L

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W i s 8 J a n n e 7. E 1 s t n e r a h APPENDIX B - ^ A a s O e DISPLACEMENTS i a t e a i 1 1 I f

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ELEVATION VIEW t i -______-

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          /                                                                                                                                                    F) t b
                                                           --______                                                                                            y Ef DUTTRELS3 N.5 '(820*)                               si EQUIPMENT

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1 PLAN VIEW g

ihlSTRUMENTATION FOR EQUIPMENT #CCESS .: ELEVATION #32'. O' k FIGURE 23 i e J e

6 { l' TADLE 23

1

                                                                                                                                                                                                                                                           -1 1:

VERTICAL DISPLACEMENTS (IN.) F + PDF.SSURE (PSIG) ' O.00 12.00 35.00 45.00 55.00 6N30 55.00 45.00 35.00- 12.00 0.00 + DATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 11/2 11/2 11/3 11/3 TIME 8.19 18.02 4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08

      ...-- ..-- =--                                                                    _ - - - - - - - - - -

GAGE ELEV.* AZIMUTH 90 0 28V 270-8 0.000 0.023 0.097 0.118 0.168 0.171 0.163 0.153 0.129 0.061 0.026 128v 267-6 0.000 0.044 0.167 0.215 0.278 0.297 0.276 0.249 0.205 0.093 0.040 164v 4111 SP RNG 0.000 0.103 0.374 0.492 0.632 0.745 0.67,7 0.567 0.458 0.199 0.073 34V DOME APEX 0.000 0.116 0.376 0.499 0.635 0.750 0.665 0.557 0.448 0.190 0.058 y AZIPUTH 200 7 V V V 29V 270-8 0.000 0.025 0.095 0.133 0.180 0.196 0.186 0'.169 0.130 0.047 0.014 f-- 129V 267-6 0.000 0.045 0.151 0.210 0.272 0.316 0.294 0.257 0.206 0.084 0.027 1 165V 4Til SP RNC 0.000 0.093 0.354 0.472 0.605 0.715 0.666 0.559 0.451 0.200 0.079 5 34V DOME APEX 0.000 0.116 0.376 0.499 0.635 0.750 0.665 0.557 0.448 0.190 0.ws. I 2 i AZIMU1H 333-55 '& 30V 270-8 0.000 0.029 0.096 0.127 0.166 0.192 0.182 0.159 0.128 0.0 56 0.020 I 130V 267-6 0.000 0.044 0.157 0.210 0.266 0.308 0.289 0.249 0.201 0.090 0.035 , 166V 4Til SP RNG 0.000 0.081 0.359 U.481 0.620 0.731 0. 6 , . 0.559 0.473 0.212 0.087 g 34V DONE APEX 0.000 0.116 0.376 0.499 0.635 0.750 0.665 0.557 0.448 0.190 0.058 {;. w I E

VERTICAL DISPLACEMENTS ARE FROM BASE SLAB EL:V. 93-0 TO ELEV. 3110KN ,

9

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                                                                                                                                                                                                                                         ;L
                                                                                                                      -TABLE 24 s

CYLINDER WALL RADI AL DISPLACEMENTS (IN.) -

V y

          ..                      _ _ _ - . . - - - - -                     _ . . - - -----        ..--=-                                   . . - - - - - - - - - - _ - _ . - - . _=..--....--_ - -.....-------. ...--

PRESLURE(PSIG) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00

DATE 10/31 10/31 11/1 11/1 11/1 11/2 11/2 '11/2 11/2 11/3 11/3 TIME. 8.19 .18.02 4.04 '11.48' . 19.11 2.41 9.25 14.39 19.58 6.00 12.08

                                                                                                                          ---__=_- --.-

CACE ELEV. AZIMUTH 90

             -1                                     98-0             0.000         0.003        v.019             0.024             0.028          0.031              0.030           0.026       0.022         0.012     0.007                   '

4 108-0 0.000 0.015 0.069 0.009 0.109 0.124 0.115 0.096 0.079 0.036 0.014 D 7 140-0 0.000 0.026 0.110 0.139 0.159 0.175 0.163 0.132 0.107 0.043 0.007 10 172-0 0.000 0.024 0.064 0.092 0.136 0.171 0.171 0.16 5 0.139 '4 0.068- 0.035-13 20 4-0 0.000 0.002 0.028 0.048. 0.077 0.087 0.066 0.000 0.062 0.005 -0.022 A 16 236-0 0.000 -0.001 0.003 0.016- 0.042 0.062 0.064 0.064 0.044 19 246-0 0.000 -0.001 -0.039 -0.045 -0.059 -0.049 -0.047 -0.046 -0.043

[I 4 22 253-O' O.000 -0.002 -0.044 -0.051 -0.064- -0.053 -0.051 -0.0 50- -0.046 -0.029 -0.028 25 267-0 0.000 -0.020 -0.079 -0.089 -0.111' -0.114 -0.107 -0.101 -0.076 - 0.052 -0.038 h 128 270-8 0.000 -0.034- -0.088 -0.101 -0.121 -0.120 -0.099 -0.077 -0.072 - 0.057 -0.047 6 Y

AZIVA3 200 L( g-2 5 98-0 108-0 0.000 0.000 0.000 0.015 0.017 0.067 0.024 0.084 0.031 0.038 0.106 0.038 0.103 0.0 38 0.092 0.038 0.031 0.024 )- 0.097 0.082 0.039 0.013 6 8 140 0.000 0.039 0.128 0.173 0.210 0.244 0.237 0.206 0.168 0.080 0.035 - i ; 11 172-0 0.000 0.034 0.102 0.155 0.104 0.705 0.186 0.178 0.138 0.053 0.015 i 14 204-0 0.000 0.014 0.054 0.099 0.110 0.130 0.136 0.130 0.097 0.028 -0.001 l-17 236-0 0.000 0.022 0.044 0.075 0.094 0.114 0.097 0.091 0.066 0.013 -0.008 , 20 246-0 0.000 -0.010 -0.021 -0.002 0.011 0.026 0.027 0.028 0.038- 0.024 0.010 I 23 253-0 0.000 -0.007 -0.025 -0.012 0.000 0.011 0.012 0.014 0.019 0.006 0.003 ' 26 267-0 0.000 -0.024 -0.052 -0.064 -0.076 - 0.071 -0.062, -0.046 -0.008 0.048 0.053 l 129 270-8 0.000 0.003 -0.001 -0.003 -0.002 -0.004 0.0I5' O.018 0.021 0.026 0.027 g b AZIEUTH 333-55 h ( 3 98-0 0.000 0.002 0.018 0.024 0.031 0.036 0.036 0.036 0.032 0.020 0.015

             '6                                    108-0             0.000         0.016       0.052             0.069             0.085           0.098              0.092          0.080        0.065         0.028     0.008             ;

9 140-0 0.000 0.037 0.111 0.147 0.183 0.211 0.194 0.166 - 0.134 0.056 0.015 12 172-0 0.000 0.034 0.098 0.131 0.171 0.195 0.179 0.164 0.134 0.059 0.020 lb 204-0 0.000 0.000 0.044 0.074 0.104 0.127 0.127 0.127 0.101 0.038 0.008 18 236-0 0.000 -0.000 0.026 0.054 0.076 0.076 0.078 0.082 0.090 0.045 0.023

21. 246-0 0.000 -0.010 -0.007 0.005 0.024- 0.039 0.042 0.047 0.055 0.026 0.017 s-24 27 253-0 267-0 0.000 0.000

                                                                                 -0.011 0.028
                                                                                              -0.032
                                                                                              -0.077
                                                                                                          -0.029
                                                                                                          -0.078
                                                                                                                                -0.016-
                                                                                                                               -0.015
                                                                                                                                                 -0.007
                                                                                                                                                 -0.031
                                                                                                                                                                    -0.004
                                                                                                                                                                    -0.071 0.001
                                                                                                                                                                                    -0.049 0.011
                                                                                                                                                                                                -0.019 0.011 0.019 0.008 0.029         -p[

130 270-6 G.000 L.000 -0.014 -0.011 -0.002 -0.007 -0.002 0.001 0.005 0.002 0.000 [ 4, t l h l _

4 . !. . 4 e , P I^m 25 EQUIPPENT HATCH VEI!TICAL DISPLACEMENTS (IN.)

                                         ==                         --
                                                                                                                  -.        =                       ==        ......

PEESSUEE(PSIG) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.00 12.00 0.00 DATE 10/31 30/31 11/1 11/1 11/1 11/2. 11/2' 11/2 11/2 11/3 11/3 g. TIME 8.19 18.02 4.04 11.48 19.11 2s41 9.25 14.39 19.58 6.00 12.08' }

             .......... ..............=-           . .- = __-___-                    _
                                                                                                                                  - _ - - = .............

GAGE A2. ELEV. 48V 150 163-0 ~0.000 -0.002 0.048 0.054 0.061 0. 051 0.051 0.057 0.054 0.036 0.023 ,: 4 7v - 150 159-0 0.000 -0.003 0.065 0.075 0.085 0.067 0.067 0.073 0.069 0.042 0.027 46V '150 155-0 0.000 0.000 0.065' O.073 0.004 0 . 06 0 0.067 0.071 .0.072 0.049 0.033 45V 150 151-0 0.000 -0.003 0.041 0.044 0.050 0.C38 0.041 0.045 0.044 0.028 0.017 44v 150 147-0 0.000 -0.004 0.055 0.059 0.066 0.051 0.054 0.061 0.060 0.041 0.028 [- b 43V 150 144-0 0.000 -0.003 0.038 0.040 0.047 0.035 0.037 0.041 0.040 0.028 0.021 . 35v 160 132-0 0.000 0.001 0.026 0.030 0.035 0.03G 0.035 0.034 0.030 0.016 0.010 y 36V 1 50 120-0 0.000 -0.003 0.020 0.023 0.02G 0.024 0.026 0.026 0.025 0.013 0.007 *

42V 139 132-0 0.000 0.000 0.024 0.028 0.032 0.032 0.032 0.032 0.032- 0.032 0.026

[. e 41V 137 132-0 0.000 0.000 0.026 0.030 9.034 0.033 0.033 0.033 0.030 0.019 0.013 ; 40V 134 132-0 0.000 0.001 0.028 0.033 0.u38 0.038 0.037 0.036 0.033 0.019 0.013 g 39V 131 132-0 0.000 0.001 0.025 0.029 0.033 0.035 0.035 0.035 0.032 0.020 0.015 , 38v 126 132 0.000 -0.001 0.021 0.024 0.028 0.027 0.027 0.027 0.026 0.016 0.011 t I 1 t I v 5 t

4 e s' t t i 7 Al? LC 26 ECUIFMENT HA1CII RADir.L CISPLACCF EN1S (IN.) 3 PRESSURE (PSIG) 0.00 12.00 35.00 45.00 55.00 63.30 55.00 45.00 35.C0 12.00 0.C0 CA1 C 10/31 10/31 11/1 '11/1 11/1 11/2 .11/2 11/2 11/2 11/3 11/3 . TIMC 8.19 18.02 4.04 11.48 19.11 2.41 9.25 14.39 19.58 6.00 12.08 k _ _ _ _ _ . - - - - - - - - - = = = = - - - - - - _ = = = CAGC AZ. CLEV. 35 160 132-0 0.000 0.022 0.057 0.071 0.097 0.110 0.096 0.024 0.071 0.037 0.019 2 36 150 120-0 0.000 0.010 0.04. 0.050 0.065 0.069 0.061 0.055 0.050 0.429 0.019 N 42 139 132-0 0.000 0.022 0.0 5', 0.068 0.094 0.108 0.091 0.074 0.062 0.033 C.014 43 150 144-0 0.000 0.008 0.026 0.028 0.044 0.049 0.044 0.039 0.034 0.012 0.003 (; L 42 139 132-0 P.000 0.022 0.05) 0.068 0.094 0.108 0.091 0.074 0.062 0.033 0.014 41 137 132-0 0.000 0.020 0. 0 6,? 0.072 0.097 0.109 0.095 0.078 0.066 0.033 0.015

I 40 134 132-0 0.000 0.025 0.079 0.095 0.128 0.145 0.134 0.113 0.097 0.055 0.031 l 39 131 132-0 0.000 0.032 0.089 0.108 0.139 0.157 0.142 0.120 0.103 0.053 0.024

y 38 126 132-0 0.000 0.038 0.110 0.138 0.182 0.208 0.1E9 0.159 0.136 0.068 0.030

43 150 144-0 0.000 0.008 0.026 0.028 0.044 0.049 0.044 0.039 0.034 0.012 0.003 44 150 147-0 0.000 0.0C9 0.025 0.026 0.043 0.047 0.047 0.044 0.038 0.018 0.009 45 150 151-0 0.000 0.015 0.032 0.035 0.054 0.057 0.052 0.050 0.043 0.020 0.009 46 150 455-0 0.000 0.018 0.044 0.048 0.07C 0.071 0.060 0.052 0.052 0.022 -0.005 47 150 159-0 0.000 0.017 0.041 0.047 0.073 0.077 0.073 0.070 0.060 0.023 0.013 48 150 163-0 0.000 0.025 0.052 0.061 0.094 0.101 0.066 0.081 0.069 0.02u 0.010

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REACTOR BLDG. LOCATION RRD1RL . LOCATION No- I CHANNEL 4I7 INSTRUMENT No 24 AZIMUTH 92 . ELEVATION 98-0 TEST PRESSURE P= 63.3 PSIG 7 '

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REACTOR BLDG. LOCATION RRDIRL LOCATION NO: 2 CHANNEL 427 INSTRUMENT No 64 AZIMUTH 200 . ELEVATION BB-B TEST PRESSURE P= 63.3 PSIG 70 , 7 ,,,,,,,,,

                                   /                -
                                                        - -PREDICTED 65                       /           -
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                                                            /              -     PREDICTED 65                                  !
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                                                                                                                                                                                            . ~ usa REACTOR BLDG. LOCATION                                                  R19D I FIL LOCATION NO-                           4                      CHANNEL                           4IB                   INSTRUMENT NO 42 AZIMUTH                   BB                                  ELEVATION                            IBB-B TEST PRESSURE P= 63.3 PSIG 7                                     ,

7 ,,,,,,,...

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                                                              /                              -  PREDICTED 65                                 I                                                                                            '
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REACTOR BLDG. LOCATION RRDIRL LOCATION No- B CHANNEL 429 INSTRUMENT No E4 AZIMUTH 2BB ELEVATION I4B-B TEST PRESSURE P= C3.3 PSIG 70 7 ,,,,,,,,,

                                                           /                             PREDICTED                     3 83     .

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REACTOR BLDG. LOCATION RRD1RL LOCATION NO- 9 CHANNEL 439 INSTRUMENT NO- E7 AZIMUTH 333-EE ELEVATION I40-B TEST PRESSURE P= 63.3 PSIG 70 ...... ... [ PREDICTED - s , 65 l

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                                                /                             PREUI$$U s 65                        /

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REACTOR BLDG. LOCATION RRDIRL~ LOCATION NO- II CHANNEL 43B INSTRUMENT No EO AZIMUTH 220 . ELEVATION I72-B yTEST PRESSURE P= 63.3 PSIG 70 '

                                                       /                         'PR$0kTND- s s 65                              /                           IIIIIIII                                   \                                                       '

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                                                     /                        'RLDMTED P                                   3                                                                       l 65                          /                                              lll                        5"                                                             I'
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z .. . , - - a ... .. REACTOR BLDG. LOCATION RRDIRL LOCATION No. 13 CHANNEL 42I INSTRUMENT No EE AZIMUTH 90 ELEVATION 204-0 yTEST PRESSURE P= 63.3 PSIG 70 '

                                                                   /                                    PR$ DICT $D-                         s s

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                                                            /                                 PREDICTED                   s 65                             !
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             .. . ;.              ,           . . . . . - _ . - ~ . -                                               .                                                     . . . .       . +c.w.u.x REACTOR BLDG. LOCAT'ON                                                    RRDIRL LOCATION NO-                        1E                          CHANNEL                                  HbI                    INSTRUMENT NO 83 AZIMUTH                  333-EE                                 ELEVATION                                2E4-0 yTEST P ESSURE P= 63.3 PSIG
                                                       /                                      PREDICTED 33                           /                                                Illlll3 i

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REACTOR BLDG. LOQATION RRD1RL LOCATION NO- 1E CHANNEL 422 INSTRUMENT NO- BE AZIMUTH 90 ELEVATION 235-0 7 TEST PR SSURE P= 63.3 PSIG

                                      /                         PREDICTED.

65 / l l ll " 1 l L.-.l. l

                                                                      !.       L .LL.9 L (;' I         .l   L L11. .!    ' l-       I                  ' ''

l 60 I / 55

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l - 50 .

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! DISPLACEMENT (INCHES) l 3-23 i4

                                                                                                                                                                      .,.+         >.u,nz-s. ,x:
      . REACTOR BLDG. LOCATION                                                    RRDIRL LOCATION No,                    17                             CHANNEL                             432             INSTRUMENT No_ l E AZIMUTH            299                                    . ELEVATION                               235-9 EST PRESSURE P: e3.3 PSIG

[ PREDICTED - s s5 / I I II II \ _ ___. a n._i , i i i gi ii i,, 4 .i ., i i. .. . I I l l 60 /

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                                                                                           /                                                                                                                  ~

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x ( 25 i 20 l l f I J' , 15

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                                                              . DISPLACEMENT (INCHES) 3-2h
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                       . . _ . . - . . . - .                                = - - .                                                                                 .
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REACTOR BLDG. LOCATION RRD1RL l IB LOCATION NO. CHANNEL 442 INSTRUMENT NO 79 AZIMUTH 333-EE ELEVATION 225-M y TEST PRESSURE P= 63.3 PSIG 7 , ,,....... l

                                                                               /                          PREDICTED                    s                                                                                  !

cs / IIII II I l i i t.. . i i ii i li

f. c _ .L .L U. .L .U 8 1 J. J ._u U_ J..u.L I

80

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                                                                                                                                                   )_.-        ._   . _ . __

l - 50 g l J 45 _. _ . _.._ _. __ _

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.- . . - - . = . e2:a.u.n l l 4 REACTOR BLDG. LOCATION RRDIRL LOCATION NO- I9 CHANNEL 423 INSTRUMENT NO_ EB AZIMUTH 92 ELEVATION 245-B TEST PRESSURE P= 63.3 PSIG 7 f - PREDICTED Y 65 ., i t._1 _ gt i it i iiii it'i i eri i, i 60 , 55 --> - -- - -- ~~ - -- .- --- -- ---- - - - - -- - - - - .-~~ 50 t I l 43 _. ____ _ . ._. _. _. __ _ - 2 m

o. 40

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l llll y . 35 _ . __ ___ _ __ ____ LIMIT

w. _._. _ __ _ __ ___ ._.._. __ _ ._ . _ _

a M y 30 ) a: I a. 25 20 1 15

'(

_.l p. l l l ll l ll l -~ l l l llll llll 3 n T d i mi iiii un W 5

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0.5 DISPLACEMENT (INCHES) 3-26 ,

     . - . - . . -        - . - - - -                                  . . .                    -               ~        ~                     w ,     m a.+x=wn.wrun l

! REACTOR BLDG. LOCATION RRDIRL LOCATION No. 2B CHANNEL 433 INSTRUMENT No 7E AZIMUTH 202 - ELEVATION 245-B TEST PRESSURE P= 63.3 PSIG 7 l

                                                   /                                <

M dEf$D 65 / / I! I i ti i i 44i _ ii . i iiii i ii i it iii itii sii.

60 /

                                                             /                         f ll'                         .

55 - - __ _ _

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50 I lill f LIMIT 45 ~ 4 n > i $ \ S /

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                                                                   \                                                                                                      .

I y 35 __. _ _ __ ____ __ _ _ _ _ _...._ _ _ __ _ ___ _ _. _ _ ._ l a in CO 30 ' IJ! l I C t O. 25 i 20 .

                                                                  'I 15

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0.3 0.4 0.5 DISPLACEMENT (INCHES) 3-27

x .; m. u m ammwa4r..m. REACTOR BLDG. LOCATION RRDiRL LOCATION NO. 2I CHANNEL 443 INSTRUMENT NO 55 AZIMUTH 333-EE . ELEVATION 245-0 TEST PRESSURE P= 63.3 PSIG 70 7 .......

                                            /                            e   -

PREDICTED 65 / 2 lll l _ .- J. _. L ._ 1. 4). +)' . ._1 . L ._ 1 J.

                                                                                        .                                  '. .L. .U_L __L_._Li.u.              _Lui l

60 55 .--.4-. -- - = [ -. - - -.--- --.-_ - - - - -- - 50 i -

                                                                                        - LIMIT f

43 _. ____ _ . ._. _ _.. . . _ ..._. _ __ __ _ _ _ _ _ . _ . ._ _ _ _

       ^                                                               :

(D

       -                                                                                                   l I

35

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(n ' CO 30 I 1 U.J u . l Z j I O. ' E' , l ! 20 l l { 1 15 l l l l - l ll !!! io u i u i u! iT i i ni ni 1 :. t

                                                '          I 5

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+ .

 .                     .                                  -         . . . -          --         -.          -_         .=x:        .+ ; a a w .: n -a m m .

REACTOR BLDG. LOCATION RRDIRL LOCATION No1 22 CHANNEL 424 INSTRUMENT No 83 AZIMUTH 92 ELEVATION 2E3-0 TEST PRESSURE P: 63.3 PSIG 7

se h _ __ J. g.:1. . .. .L .!. J. J. _ ._ .L_.,_ L . _!. L!. ' '

                                                                                                                                       ' !J .J LL_ J.L .L J          1                                                                                                    -

60 ' ( N PREDICTED i 55 ~ ~- l-l - -- - -l -l -l - -- -- -- - - - --- - - - - ---- 50 k

i 45 -- --- - -- - - -- -- - -- - - - - - -- ---- - - n SE E 40

   -                              l                                               1llll g                            i         {

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                             --y A-                                                                                                             l o                                         /                                                                                                                   1 m                                                                                                                                                              1 M   30                           -

I - W i ) x \ Q. ' 25 f \ 1 20 ' I I 15 k . _.._ __ _.! _ . I..__ _. ._lll l l l ll lll q lll t 5 f 0

       . - O. I                              O.0                               0.1                 0.2                   0,3                 0.4             0.5 DISPLACEMENT (INCHES) 3-29

      -        ._         .                             ..                  .        - - .                .- . = _ . -             a .                        +        + ~ - _ .                        -  , - . .

REACTOR BLDG. LOCATION RRDIRL LOCATION No. 23 CHANNEL 434 INSTRUMENT No_ 21 AZIMUTH 250 ELEVATION 2E3-0

j. TEST PRESSURE P: 63.3 PSIG s

65 ' / _ __ J. bg1. ._! .! .!. J. U. _ .L.!.'_ ui l' i i u.L.! u i__ J. , .J_u. _!.q1 _ l 60 . 55 .._.._. _q _. _. ._ _ _ _ . _. . _ _ ._ _ _ . _. _. __ _ _ _ __ ._. _ _ _ _ ._ . _ _ 50 45 _. ___._. ._. _ O ! 25 - - -- LIMIT

a. 40

( / l 35 . _._._._ , _ , _ m CD M 30 1J.1 Q: O. 25 20 'I 15 ll _ ll _ l _. l lll l l lll' I IO tI Il i II i l lli I il I 11 ll I till I 5 O h

                                - O. I                         O.0                               0.1                  0.2                          0.3                         0.4                     0.5 l

l DISPLACEMENT (INCHES) 3-30 1* - . . - . . . .

                                -                     - .. . .~. z : .            .        a_      -        .- - =. -            x.wn              a. wu..

REACTOR BLDG. LOCATION RRDIRL LOCATION NO. 24 CHANNEL 444 INSTRUMENT NO 74 AZIMUTH 333-EE ELEVATION 2E3-B 7.-TEST PRESSURE P= 63.3 PSIG 65

            .   .. i   ft..          I
                                                            .L J.    !. _ _. .L _    L   1.     '
                                                                                                     .L J.LI'      I-       ' Ll.J L L!. J..L.L 60 l                                                                                                                       l l                                     l i                                     I               -

55 -.- --- - 50 f 45

I w 55 40 i o,, Illl u.s 33 -_ ... l _. _

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j 3 / m } ! m 30 l- i to a

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25 - t 20,I , i't 15

                                              .'                                      ll                      l       ll           l             ll 10 l             '                 I           II'                  Ili     I  Il    !    I!           I  I    I
                                            \

5 O I

        - O.I                           O.0                             0.1                0.2                0.3                  0.4                  0.5 DISPLACEMENT (INCHES) 3-31

               -            .                  .. .: - -          . . a .c :u-                 ..u_.~.=.~-                            , _ , . . . . . . . ~ ,
 --      REACTOR BLDG. LOCATION                                RRDIRL LOCATION No.                   2E                 CHANNEL           42E           INSTRUMENT No 99 AZIMUTH            99                             ELEVA TION         2E7-9 TEST PRCSSURE         P= 63.3 PSIG 7o
                                                   /

Ii

                                            /                                  ,

65 I

                            ._gI__ g j J_lg _L _L _L _L L    JJ    l__   JJ '         '     '    '         '      '

PREDICTED l 6o I

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                              .                            DISPLACEMENT (INCHES) 3-32 w  .,--       ,

       -     .-                   -                           -:....~.                                       - - - .
                                                                                                                                                        -c-.-.             .                                                          ,.u.n-nanu
   . REACTOR BLDG. LOCATION                                                    RRDIRL LOCATION NO.                             25                        CHANNEL                    43E                       INSTRUMENT No                                                                                              IB AZIMUTH                 222                                      .

ELEVATION 257-0 yTEST PRESSURE P: 63.3 PSIG

65 ' Iq _L lt L._11 J. J. _ L1_ L LJ 1 _!. ' L .L '' !. !J._!.L L!. q , i I 60 55 . _.. ..j. __ __ __ _ __. - . _ ._ _ _ . _.- __ _ _ _ __ - 50 k , , 45 - - - --- - - -- - - -- ~ ~ - - - -- ---- --

l E '

40

                                              .lj                                             i                                                                                                                                                              :

l g 35 ._

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                    ,3

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l DISPLACEMENT (INCHES) B-33 l l l l l

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4

 . REACTOR BLDG. LOCATION                                                         RFID I RL LOCATION NO.                          27                                CHANNEL                    44E                 INSTRUMENT NO. B2 AZIMUTH                 333-EE                                      . ELEVATION                      257-2 TEST PRESSURE P= 63.3 PSIG 7

IPREDICTE

l' l 65 - u l l , LJ. _!. _!. .L' ' ' h ._. _.it._ . ._ J. .. c_ ._ L U..L -

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                                                                                                                                                                 .JpL!. _!. .U .'.

l 60 4, l I i l 55 - 50

                         \                                                                                                                  l
                         .I                                                                                                                 l 45   _.          __       _   . . _ . __      __     _.     ._  _              .. . _ -   _._      __

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B-34

 . . . . ..  .-           .=            -..             .. ~ n..     .

_ _ . _ . .=.-.- .

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1 REACTOR BLDG. LOCATION VERT I CFIL LOCATION No. 28 CHANNEL 40I INSTRUMENT No 72 AZIMUTH 90 ELEVATION 270-8 TEST PRESSURE P= 63.3 PSIG 7 ,.. ......

                                                    /                                                                          -

PREDICTED 65 I I

                                              .1 L ._ 1 .!. _!. .1_                                             L                                         :

f_1 .!. p ' ' U .U ' ' ' ' 60 I / l 1 . 55 l W < So l /l l / j ,

                                                                                                 /                           /
                                                                                                                               /                                                               \

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LIMIT x - o l m M 30 / / I W / l m Q. 25 ' /

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                                                                  /           /

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0.1 0.2 0.3 0.4 0.5 DISPLACEMENT (INCHES) 3-35

   -           .-...:...                                        =.                   -
                                                                                                                              .          ..          .      a , , . . m. a. .

REACTOR ' BLDG. LOCATION VERTICRL L'OCATION No- 29 CHANNEL 407 INSTRUMENT No EI AZIMUTH 200 ELEVATION 270-8 TEST PRESSURE P= 63.3 PSIG 7 . i. . i.i

                                      /                                                           p!l.'                    PREDICTED 33                          /                                                          .si             /-          lllll       111-1 J. L .JJ L!. ' ' '1
                           ' ' 1'. . .!. .!. J. L!.
                                                                                                            ._@-          J.$.Li.! ' '

60 ) l l \ 55 ....._. _. _. .._ _ _ . - _. _ . _ ... -. . _ j 50 /

                                                                                             /       '
                                                                                                                 /
                                                                                        /                     J 4s  ..   ---.       ...-.       -. _ .   ..            ..

4r . j i J E 4 t i j ijj

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[ 35 -- .-- -- --- - _ _

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25 2

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20 ) l l l tl I I l

                                                    ;/ /                     /

i 15

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                                                                                                                 !l
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         - O.1                       0.0                              0.1                                0.2                      0.3                     0.4                        0.5 DISPLACEMENT (INCHES)                                                                                                                    ;

l 3-36

P-w,wwme

meDe-'mm e-e9 ee-O M"%M w%w =M^ 'M' 452& & a& AJ ' em -M6h 's Y ,h& -

d h. *. i REACTOR BLDG. LOCATION VERTICRL LOCATION Nd 30 CHANNEL 412 INSTRUMENT NO- 90 AZIMUTH 330-EE . ELEVATION 270-B TEST PRESSURE P= 63.3 PSIG 7

                                                               /                                                                                  -    PN$ DINE'D'
                    .65                                      l                                                                               1

_ .. _1. _1. L ._

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                                                                                                                                          ._? _ .L ._ p. .L
                                                                                                                                                                                                 -   .1   _   . J Lu. _!..L' .!

60 h / I f 55 -- --- -- -- --- -- - .- - -- (i '

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50

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b Y Y (,' l l ll w 35

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                                                                                                                                                         -- L.IMIT g

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                                                                                                        /                  /

f IJ.! 30 r t y E ) ) O. f 25 l '

/ /

20 . I I Y f f l 15

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                                                                         )                 f
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-. - . . - . . . _ - . = . . ~-

                                                                                        .- ,                       . . . .                       . - .               . .      ~~m               ~ w s ,~..

l 1 1 REACTOR BLpG. LOCATION VERTICRL LOCATION No_ 34 CHANNEL 424 INSTRUMENT No- 13 AZIMUTH - ELEVATION DOME RPEX TEST PRESSURE P= 63.3 PSIG 70 - 7 ,i,,,i,,,, PREDICTED 65 /

lill Illi s\ - l

                                     .. ___.        JI     i     liti       '      i
                                                                                                 ' LL                           i-           ii        i .LJ.!. J .L .J_.J.22.u.L2                    __      ,

60 l/

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jf, f i

                                                                                                                                                             #y /

i .\ ' 55 - -- --- - -

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So l / /- j' / f

45

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9 m

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15

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l

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                                                                                                                                                                               ~
                                                  .                          DISPLACEMENT (INCHES)
                                                                      ,,                             B-38

                                                                                                                                                                             = _ _ _ _         _ .        . _ - _ - _

_ -. _ _ . . __ _ _ . . _ _ _ . . _ _ _m _m REACTOR BLDG. LOCATION EGU1P. HRTCH RRDIRL LOCATION No- 3E CHANNEL 45I INSTRUMENT No E3 AZIMUTH IEB ELEVATION I32-0 TEST PRESSURE P= 63.3 PSIG 7 iiieiii.i f

                                           /                                        -. PREDICTED 65                        /                                        !    I      II!! III
                                     't           I      '     I       '

f 7 g_ ,_L !' ' ' t ' ' u. _!..U.L 60 55 .._.... __ _ .. _. ..._ f , 50

                                                                       'l   f 45  _. ____       _ . ._.      . _      _.

jA / ..._ . . _ . __ _ __ _ _ _ --

          ^                                                          l          f m    m                                                  J           /                                                                                   -
          -                                                      I          L F*- ---

ll l: I J g 35 _ .._ ._ __ ___ __ _ i

                                                                                              - LIMI.T a_,_.._                _.     ._. __.                     . __    -     _ __.      ____.._.._.._

0 y 3o 0 c 25 l ll , i 20 I I - 15 Y 7_. , 5 0 i m

               - O. I                    O.0                                0.1                      0.2                            0.3                                   0.4                      0.5
 ~

DISPLACEMENT (INCHES) B-39

REACTOR BLDG. LOCATION EEUiP. HRTCH VERTICRL LOCATION No- 3E CHANNEL HE3 INSTRUMENT No 77 AZIMUTH IEB ELEVATION I32-0 TEST PRESSURE P= 63.3 PSIG 7 ii.. .iiii -

                                   /                                         PREDICTED
                                 /                                 >
                                                                     /     I        HI'      'IIl 65

_ ___. _.. .1. ._ .. _. _'. f_g..._' ,_ i ' ' ' .L 6' ' ' ' LL f.L .L i 60 55 -->.-- - -- --- ~ ~ -'-- - - - -- ---- -- -- - - -- - - ~ ~ ---- i 50 , 7 43 -- ---- ---- - -- -- -- f O - M 40 0. I

                                                                  ,-. .IlliI l'                                      ' LIMIT 35 s                                                                                                                         I m

(n 3o I I La 0: 25 f 20 , 15 I I I l } l? ' I l 10 5 0 'C

          - 0.1                   0.0                            0.1                      0.2                          0,3                  0.4             0.5 DISPLACEMENT (INCHES)

B-40

REACTOR BLDG. LOCATION EEU1P. HRTCH RRD1RL LOCATION NO. 35 CHANNEL 452 INSTRUMENT NO 93 AZIMUTH IEE ELEVATION I20-B TEST PRESSURE P= 63.3 PSIG 7 , 7 ,,,,,,,,,,

                                           /            ,
                                                                                  ,   J PREDICTED
                                         /                                   /           l           l 33

_ ___. . ...L ._ __

                                                                      .d     _

60 T

l .__._ 55 _. _. __ __ __ _. _ ._. _. __ __ _ _ __ __ __._. _ .. 50 ) { l _ _ _ 43 _. ____ _ . ._. _. _. n m (D k 1 lll l A __-- LIMIT g 33 _ ._ . ___. _ [_ 2 1. (n M 30 )' IJ.J -1 i Q' I l C1. , 4 I l 25 -- 20 / ' It 15

                                                   ]           ]

f_.._ ._ ._ l l lll 10 ( l 5 J t O I b

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DISPLACEMENT (INCHES) I , B-41 l l ,_

R$ ACTOR BLDG. LOCATIONEBUlP. HRTCH VERTICRL LOCATION No. 35 CHANNEL ME4 INSTRUMENT No AZIMUTH IEB -ELEVATION I20-B yTEST PRESSURE P- 63.3 PSIG l [ -- PREDICTED l

                                                     /                                               /          l ll l l l                                         .

33

                                                 .L.               l        '        '
                                                                                             '6_4                                     '      '            '    '   '     - JJ. _!. J..L .L       .

l 60 ] l 55 --><-- -- - --- - - -- -- - 4. - -- --- - -- - - -- - - ~ ~ ---~~ 50 45 _. ___ _.._. _. .. _. ._ n e

             ~
                       *                                                                           ]

12 ,l

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i REACTOR BLDG. LOCATION EGUlP. HFITCH RRD I RL LOCATION NO- 3B CHANNEL 4EB INSTRUMENT NO I9 AZIMUTH I25 ELEVATION I32-B TEST PRESSURE P- 63.3 PSIG 7 [ -. PREDICTED i 65 / ' lll' lll 1 J L-- _..L U. ._ ' ' L ._p .L L -..L '- f !- q). 60 I h f I l 55 --- --- -- -- --- -- - -- - ---- --. - - -- ~ ~ -- - - - - -- . - - 1 50 / ) f / '/ lI i 45 _. . _- _.._. _. _- _. -_ __ - __ l /..

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B-h3

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REACTOR BLDG. LOCATION EEUlP. HRTCH VERTICRL LOCATION No. 38 CHANNEL _ W 9 INSTRUMENT No 7 I AZIMUTH I25 ELEVATION I32-B TEST PRESSURE P= 63.3 PSIG 70 7 .......... [ -- PREDICTED 65 lll 1 _ ___. _. J. L . . .L .. _ I ' ' ' ' 60 nl 1 ( 55 - 50 , 45 _. ____ _._. _. ... _. . __ cs_ E 40 i I

                   -                                                                                           L'                    III g                  35                                                 ,

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B-hh

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REACTOR BLDG. LOCATION EGUlP. HRTCH RRI)i RL LOCATION Nd 39 CHANNEL 4E7 INSTRUMENT No B4 AZIMUTH I31 ELEVATION I32-B yTEST PRESSURE P= 63.3 PSIG

                                                                 /
                                                                                                                        -    PREDICTEG 65                                    I                                                /               !!!                                                        i             '     '

_ .._. ... .1 .._ _L _ . _ . _ 4 L L I I ' 60 ))l I / 55 --- --- -- - --- -- - -- -- -- -- -- -- - - - -- -- - ~ ~ ------

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B-h5

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l REACTOR BLDG. LOCATION - EBUiP. HRTdH VERTICRL LOCATION No. 39 CHANNEL 8-lEB INSTRUMENT No- I E' AZIMUTH I31 ELEVATION I32-B _ TEST PRESSURE P= 63.3 PSIG 70 , 7 . .........

                                                                      /                                                    ,   -   PREDICTED.

65 / / (Lll ' _ ___. _.1... _ . .. _. _. f _ _.._ ._ _!. LJ. ._. ! -- 60 [ 35 .._.._. __ _. ___. _. _.._. . _.. . . _ ._. . _ . _. __ __ _. __ __ _._ l 50 , 45 _. ____ _ . ._. _. _._. __ __ ......_. _ _ __ _ (9 J ! en I

i O. 40

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l i LIMIT 35 0

                       .tn M          30                                                                      '

id i CC I 0 25 I 20 I f 'r I 15 _.._ __ __ __ _ . . _. _.._ ._ ._ __ .__.._ .. __ ___ =- - .,_ _.= __ _. __ _ 10 j 5' l O , l - 0.1 0.0 0.1 0.2 0.3 0.4 0.5 DISPLACEMENT (INCHES) B-h6

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REACTOR BLDG. LOCATION EGulP. HRTCH RRDIRL LOCATION NO. 40 CHANNEL 456 INSTRUMENT NO EB AZIMUTH I34 : ELEVATION I32-2 TEST PRESSURE P= 63.3 PSIG 7 , 7 ,,,....,, I

                                                     /                                                  -    PREDICTED 65                               I
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REACTOR BLDG. LOCATION EEUlP. HRTCH VERT 1CRL LOCATION N 40 CHANNEL HE7 INSTRUMENT No 40 AZIMUTH __._i34 . ELEVATION I32-0 TEST PRESSURE P: 63.3 PSIG 7 [ - PRdICTNd 65 I' ! _ . . 1._ _ d _ g. ._ ._ .JLi I ' ' 'Lj. ' ' ' ' so ) 55 .._.._. __ _ __ _. .. __. .._ ._ ___ ...__ __ _ __ __ __ __ ._.._... l 50 45 _. ____ _.._. __ _ _. ._ n m a

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                       - O. I                       O.Q                                   O.1                       0.2                        0.3                              0.4                               0.5 DISPLACEMENT (INCHES)
                                                                      ~

B k8

REACTOR BLDG. LOCATION EBUlP. HRTCH RRDIRL LOCATION N6- 4I CHANNEL HEE INSTRUMENT NO_ 29 l AZIMUTH I37 . ELEVATION I32-0 yTEST PRESSURE P: 63.3 PSIG ,

                                                                           /                                                  , 3RddfCTdd 65
                                                                                                                           /            ll               l

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_. . _ _ _ _ . _ , _ .______._..m. _ 4 4 REACTOR BLDG. LOCATION EEUlP. HRTCH VERTICRL LOCATION No- 4I CHANNEL 4E5 INSTRUMENT NO IB AZIMUTH I37 . ELEVATION I32-0 yTEST PRESSURE P= 63.3 PS,IG 70 , i,........

                                                     /                                         /

PREDICTED 1 s5 / ! I I

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s REACTOR BLDG. LOCATION EGUlP. HRTCH RRDIRL LOCATION No- 42 CHANNEL 453 INSTRUMENT No 57 AZIMUTH I39 ELEVATION I32-B TEST PRESSURE P= 63.3 PSIG 7 ii+

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                                                  /                                            - -PRE'D'IC'  '

T' E' D' 65 / l J

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DISPLACEMENT (INCHES) B-51 i

REACTOR BLDG. LOCATION EGU1P. HRTCH VERT lCRL LOCATION NO. 42 CHANNEL 4EE INSTRUMENT No 79 AZIMUTH I39 ' ELEVATION I32-0 TEST PRESSURE P= 63.3 PSIG ) 7 I - N$biC$$b 65 l A \ _ .__. _ ... L ._ ._ .._ _. .. f._ _...._ .L _ _ 60 f . 55 --- '-- -- -- --- - - - -- -.- -- -- -- -.~ -- - - -- - - 50 , l 45 _. _.._. _. _. . _ __ .. .._. . __ _. _ _ __ _ _ __.._ . , _ n co 25

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l DISPLACEMENT (INCHES)

B-52 1

REACTOR BLDG. LOCATION EEUlP. HRTCH RRDIRL LOCATION NO- 43 CHANNEL 494 INSTRUMENT NO 99 AZIMUTH IEB ' ELEVATION I 44--!! TEST PRESSURE P= 63.3 PSIG 7

                                                  /                                       -      NbkbNb s5                              /                                   /            I           II     I If o'.                                                                                     '
 ,                    -   .--.        _,        1 ..-        1                          .          .  ..-                                                L -

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B-53 f

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                                                       -                                                                                                                                j REACTOR BLDG. LOCATION                                                EEUiP. HRT'CH VERT _ICRL LOCATION Nd.                       43                        CHANNEL                              ME2                INSTRUMENT No AZIMUTH                 IEB                                 ELEVATION                              I44-0 TEST PRESSURE P= 63.3 PSIG 7                                 i i iiiieii
                                                            -                                                                                                                           j
                                                          /                                -     MEDICTED l

I 65 u " ' I - ' ' ' ' ' _ ___. _ .u.1. . _ l 60 , 55 1

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B-5h . e-,-,,,

1

                                                                                                                                     .              .-.    . ~ - .       . . . . . + . . . .

1 REACTOR BLDG. LOCATION EBUlP. HRTCH RRDIRL LOCATION No- 44 CHANNEL 470 INSTRUMENT No BE 1 AZIMUTH IEB ELEVATION I47-B TEST PRESSURE P= 63.3 PSIG l 7

                                                /                                          -  -

PkkbCi$ 65 / -/ l'illlll

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B-55

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RENCTOR BLDG. LOCATION EEUlP. HFITCH VERTICRL LOCATION No 44 CHANNEL HEI INSTRUMENT No-AZIMUTH IEB ' ELEVATION I47-0 TEST PRESSURE P= 63.3 PSIG 7 , 7 ,,,, ..,,

                                   /
                                                                               -    PREDICTED
     .3
                                 /                                        /          III'l                II
           -   ._..    -..    .t         i      i                 -      2        -                                '    '         i.L          '             it       '                                     '             '

60

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p. _. - ._.- . - . - . ._ _ __ ._. -_ __ -- .-. - . _ . ._ ._ ._

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B-56

REACTOR BLDG. LOCATION EGlilP. HRTCH RRDIRL LOCATION NOl HE CHANNEL 47I INSTRUMENT No 38 AZIMUTH IEB ELEVATION IEI-2 TEST PRESSURE P= 63.3 PSIG 7 ,nsess, sus

                                                                 /                               -  PREDICTED 65                            I                                                l

_ .__. _. . . I. . ..I j - L 1 '

                                                                                                                                                  '                 '              I

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           .                                                                                              B-57                    .

REACTOR BLDG. LOCATION EGUiP. HRTCH VERTICRL LOCATION No- HE CHANNEL HEB INSTRUMENT No AZIMUTH IEB - ELEVATION IEI-B TEST PRESSURE P= 63.3 PSIG 7 f , Y b 65 / -/ IllH'lll 1 ' ' 'I ' - '

                                                                                                                                                                                                      ..L i sf ..(4...                                                                 -

6o N l

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B-58 l

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    .      - _ _ _ _ . .        ._.__.m              .__                        _ _ _ .               _ _ . _ _ _                    --

REACTOR BLDG. LOCATION EGUiP. HRTCH RRDIRL LOCATION No. 45 CHANNEL 472 INSTRUMENT No_ 2E AZIMUTH IEB ELEVATION IEE-B yTEST PRESSURE P= 63.3 PSIG [ , -PREDICTED es / / II I i

                                                                                                                                  '             i                             '

_ .__. :. . t'. ._i J. _. ...

                                                                                 /g_                ._    .L    .___        J.                     '

I

                                                                                                                                                                  . J'

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a. ' I 2s 20 ' ' '

15 l l l l 10 I l 1 l I I I l

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              - 0.1                          0.0                                  0.1                        o.2                          o,3                   o.4                     o.s l

l DISPLACEMENT (INCHES) l B-59

__. _ _ _ _ _ _ _ _ -._, . _ _ _ _. m. _ __ _ m-m .e REACTOR BLDG. LOCATION EGUiP. HRTCH VERTICFIL LOCATION NO1 46 CHANNEL 449 INSTRUMENT NO AZlMUTH IEB ' ELEVATION IEE-B TEST PRESSURE P= 63.3 PS!G 7 , 7 ,,,,,,,,,

                                             /                                           . PREDICTED
                                           /                                                 I II I I e5

_ __ . _. 1. . _ I 4 .k; L -- l

                                                                                                                    -  L   !JL L'                        1----   LU-      JLl 60                                                          \              l l

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_/, 7 _ _ . .a_ LIMIT _ . . __ _ __ __ _._ . ._. 0 (n M 30 l } i Id i T 0: 1 25 ' 20 ! ' 1( 15 l I l ... ._ ._ .. ,_ .._. __. ._ ._ l .. l l l f 5 0 Cl ._a-

             - 0.1                           0.0                                0.1                      0.2                         0.3                    0.4                   0.5 DISPLACEMENT (INCHES)

B-60,

     . . . . - - . ,           m.,.              . - - - .                         wm               .,.,ec                             _ a% u,                                     Q '- - f. L O W w .C&WfTg- W,,
  '                  REACTOR BLDG. LOCATION                                                  .EBUlP. HFITCH RRDIRL LOCATION N                      47                          CHANNEL                                     473                      INSTRUMENT No 75 AZIMUTH                  IEB                                ELEVATION                                        IEB-D yTEST PRESSURE P= 63.3 PSIG
                                                             /                                               ePREbIdNd 65                              /                                             l    l I Illl I

_ ____ _.. .t. _ j_ e ' "

                                                                                                                                                    '     I   i      l'       _L  _
                                                                                                                                                                                             '    i'      '

60

                                                                                                                                                                                                                  -1 '

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B_61

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REACTOR BLDG. LOCAT10ti EGU1P. HRTCH VERT 1CRL LOCATION N 97 CHANNEL VS B_. INSTRUMENT No ' 1 AZIMUTH IEB ' ELEVATION IE9-2 ) yTEST PRESSURE P: 63.3 PSIG

                                               /                                             Illiillili
                                             /                                                 PREDICTED
                                           /                                            ' I         IIII            I ss                                                                         -

_ _...t.. _ i e t 4 J. b _ ._ i i ii i h

                                                                                                                                                                      ' ' p. .J. .'_ .L 60                                                             \                    l                                                                            l 1                 f
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M lD 30 l- \

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25 l 20 , I ' l i 15 I 10 (' ' l 1l r > 5 0 _

            - O.1                           0.0                                 0.1                          0.2                           0.3                   0.4                          0.5 DISPLACEMENT (INCHES)

B-62

1

                                                                                                                                        - . . .      . ~ . _ ~ . . -

REACTOR BLDG. LOCATION EEUlP. HRTCH RRDIRL 1 LOCATION NO. 48 CHANNEL 474 lNSTRUMENT NO_ 53 AZIMUTH IEB ELEVATION IB3-9 TEST PRESSURE P= 63.3 PSIG 7

                                                                 -                                                  niiiiiiiii                                                                               '

1

                                                              /                                                 --  PREDICTED I        I             I!!

65 _ ___. _.. .1 ... .L _. _._ f . 3.L ._

                                                                                                                                    '8           _!.  . ...   .'   '    J. _   ._       u. J.._ .L I

60 ' 55 .._. _. __ _ ___. ..._

                                                                                                  .p    ..   ._    ._. . _  . _. __      __  __        ..           __.  ._    _ _ ._ _ . _   . .. I 50                                                                    /                                                                                                             l l

45 -- ---- -~ -- - - Y n 1 h

               ~~
   .           CO                                                                             !

40

               -                                                                       i                s'                  ll      l LIM g          35          ._     ._.       __     ____       __                          .__.       _ _ - _. .IT o                                                                      l_

en CO

                                                                                         ,i j 30                      .

l I I a: 25 b,

                                                             ',l                   ,         f' 20 u

il ) I f 15 b i _.._ __ _. _. = . .._ 10 b ' 'I I I 5 0 ' Il

                           - O. I                           O.0                                      0.1                      0.2                          0.3                0.4                      0.5

( DISPLACEMENT (INCHES) { .. 3-63

                  --+ms..

REACTOR BLDG. LOCATION EGUiP. HRTCH VERTICRL LOCATION No. 48 CHANNEL 447 INSTRUMENT No l AZIMUTH IEB ELEVATION IG3-0 TEST PRESSURE P= 63.3 PSIG 7 IIIIlllll l

                                                   '                                                -    PREDICTED
                                                 !                                              /         ' L"r 65                                                                                                                                                             '

I !. l.

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25 ) i Y f I 20 / ( [ 15

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DISPLACEMENT (INCHES) B-64

                      .. ~ u                     .. - ..                                                ,__                   . a..,+                ...___,,n REACTOR BLDG. LOCATION                                           RRDIRL LOCATION No.                       I29                    CHANNEL                       425                    INSTRUMENT NO- 9 84 AZIMUTH            BB                                   ' ELEVATION                       270-9 TEST PRESSURE                      P= 63.3 PSIG 7
                                                        /
                                                   /                 lllllllll
                                               /            H-      PREDICTED I            #           '

65 _. __ . JI _ J4s . . .. .. _ _LL ' ' -

                                                                                                                                                                                 ' lJ.1 60   --

3 i 33 _ . ._ l._ l 50 i 45 = _ . ,_... _ _..___ ..._ _ _ . . .._ _ . . .. . _ _ _. _ . . _ .__ __ _ _ . _ _. n e_ E 4o x' ll w 35 I LIMIT T D U) M 30 w , 1 1 l 25 1 l 20 - l k l 15 l -- l l _ l _. -- lll 10 l

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k l l

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             - 0.2                               00    .O                 0.2                      0.4                         0.6                            0.8                       I.0    1 1
                               .                                DISPLACEMENT (INCHES)
                                                         ,,                            B-65

REACTOR BLDG. LOCATION VERT lCRL LOCATION NO. I28 CHANNEL 402 INSTRUMENT NO 25

        . AZIMUTH                 BB                                ELEVATION                                257-5 TEST PRESSURE P 63.3 PSIG 70                           ,

7

                                                  /                                                                                                   I
                                                /                                                                                    PREDICTED-- -s                       -

65 _ ___. .. .t.._ i i i i , _J. ' '

                                                                                                                                                                         .p                   ' ' .L 60                                                                                                                        l                       /
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55 ,i , L - ~ ~ <- --~ 50 ) '

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B-66

                                . _ .          . ._.                  . ~ _...

REACTOR BLDG. LOCATION VERT I CFIL LOCATION No- 129 CHANNEL 408 INSTRUMENT No 90 AZIMUTH - 220 ELEVATION 157-5 TEST PRESSURE P= 63.3 PSIG. 7

                                                         /
                                                       /                                                                                       PREDICTED --s, 65

_ ___. . ...t ... ._ -. _. _. _ ._ L.._ . '_ .___ .L J. . . . . y - gd ' l' ' 60

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45 _. ____ _.._. _. _ _. __ - .. _. _. _/ __ _

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DISPLACEMENT (INCHES)

                                                                                                       . B-67 w

1 REACTOR BLDG. LOCATION _ RRD I RL LOCATION No. I29 CHANNEL 43E INSTRUMENT No BE AZIMUTH 200 . ELEVATION 27El-B TEST PRESSURE P= 63.3 PSIG 7

lll1lllll1

                                                                                                  -     PREDICTED 65                              !                   /             '       '                                                                  *
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W I l CE i D. 1 i 25 20 Il 15 I ll__ _ l i i 5 i

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l . 1 l DISPLACEMENT (INCHES) I . B_68 i 1 l

 "-M"-   * * -   i-.me=        n-,-rwwm -e         ,,_pm.,           , _ ,

_ . _ . - _.._. ,s RRDIRL

    /  REACTOR BLDG. LOCATION LOCATION No-                                    13B                       CHANNEL                                445                         INSTRUMENT No 98
       ' AZIMUTH                         333-EE                                  ELEVATION                                 272-2 TEST PRESSURE P: 63.3 PSIG 7
                                                                   /
                                                                /
                                                          /-                    '
                                                                                   -  . PREDICTED 65                                                                   -              '
                                                       .y._ .L f g _.'                -              . . .L         . .._

8i .L J. . . .'. .LLLL. !.J- ._'_L !. !..L .L 6o 55 .--.<-- -- -- ---- -- - - - --.-- --' - - -. -- -- - - -- - - - - -~~<- h So ! 45 _. ____ _ . ._. _{ . _.... ._ .. _ . ._. __ __ _ _- _ _ . ._ _ _ m to_ ( E

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LIMIT g 35 . u 2 . (n M 30 hJ (2* Q. I 25 2o i > l l i 15 lll

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5 l I o i

                           - o.I                              o.o                                  o.i                        o.2                              o.3                        o.4                         o.5 DISPLACEMENT (INCHES)

B-69

                                                              . ~ . .                    ,

REACTOR BLDG. LOCATION VERTICRL LOCATION No. I30 CHANNEL 4I3 INSTRUMENT No B i AZIMUTH 333-EE ELEVATION 257-5 TEST PRESSURE P= 63.3 PSIG 7

                                                                        /                                                                                       I
                                                                      /                           I,                                                              PREDICTED                  ._

__s. 33 I 1, . . J. p ' ' '" 60 / /

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ss ..... . _. . ..._ __ ._..... .._. _ _ _ .. _. ._ __ _. _ /._ _. _ - .__. .-

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      , _../                             - 0.1                          0.0                                 0.1                              0.2                              0.3                            0.4                             0.5 DISPLACEMENT (INCHES)

B_TO

REACTOR BLDG. LOCATION VERTICRC LOCATION NO. i54 CHANNEL 423 INSTRUMENT NO- 59 AZIMUTH BB ELEVATION 4TH EPRRY. RING TEST PRESSURE P= 63.3 PSIG 7

                                                                /
                                                             /
                                                          /                                                                                                               PREDICTED - s "O                                                                                                                          '     '              '

_. ___. Jf _L .L.D ' i 8 ' ' L .L ._ _LQv_L!.1p. _ 60 'r r

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m / -j / M 30 / / w , < y

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                                               .                                 DISPLACEMENT (INCHES) i                                    .                                                                              B-71

! s* .

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REACTOR BLDG. LOCATION VE*RT I CRL

LOCATION No. IEE CHANNEL 429 INSTRUMENT No ~4~4 i 1 AZIMUTH 222 ' ELEVATION' 4TH EPNRY RING ) TEST PRESSURE P= 63.3 PSIG 70 <

                                                              /
                                                      /
                                                   /
                                                 /                                                                                                       PREDICTED                     w
                            -.    -_-.          f__ __! L1                     i       I LL           i                       i    '
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i 'i s-60 / I

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7 m m so ' >/ / / W x / / ,/ t a / / / 25 l / ,

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[ - . -- . . . . . . _ _

                 'm' e me         eg. dium' w w p pw+          Man -                  ne@r-. ha d 6. &                   g                          n-      a

_,s@4WgM a M@ en g - MWw REACTOR BLpG. LOCATION VERTICRL

LOCATION NO- I55 CHANNEL- 414 INSTRUMENT NO- M AZIMUTH 333-EE ELEVATION 4TH EPRRY RINE 1 g TEST PRESSURE P: 63.3 PSIG l 70 , ,

t

                                                                     /
                                                                   /                                                                                                                      PREDICTEDs ss                                                                                                                                                            '       '     '            ' ' Q)!.lJ.ip_
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                                                                                                              ,                                                                            Yf                                         l 60
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55 - .- .-..- ... _ ,_ ._..- .- _. - . _ . -- - -.._ . - . . _/ A. -_

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                                                                                        -- - ---+     wn m,

oc -, 4 mL- 49.*' 9 -

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9 O e D W ' i k J a ' R R e E I ' s t i A s f 1 APPENDIX C a TE}fERATURE DATA 9 I e e t e 1 l senr wn . :,+n . , - - , _ swa N~" - -- Tv-m -ma -.- , _ --, -- m u , a ,u . .. wm , ge:we -m ,'

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TEMPERATURE READINGS !

         ',                                                             2                                                                                          ~

DATA SHEET PAGE I 0F TEST

DATE TIME I.0 CATION TEMP. INITIAL /DATE PRESSURE NOTES to-s!*14 1013 0 Tc I27. (o4

F d60 llo-SIIL i "-m - 74 1oi5 0 rests 7 fo *F A080 natsik j to-Bt-74 IOI3 7e IZ& 72*S &Ab ih.st.7c I0-Bl
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TEMPERATURE READINGS n,

           #                                            2 DATA SHEET PAGE E       OF TEST DATE         Title                               LOCATION               TEL2P.                INITIAL /DATE PPESSURE                                                                                                     NOTES
                          /J.J-7t. 04to                        3C            7"C 12.t.            .;k> *v               &                  ///./.71.

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TEMPERATURE READINGS 2 DATA SHE T PAGE OF TEST l

                       'DATE                    TillE                                           TEMP.                                                            ms PRESSURE     l LOCATION                                    g n /D m                             .

11 - l - 7 6 1340 46 fC 122 75'F OYE /Il-I % il- 1-76 /340 46 Tc 1Z3 64 *F 11BB fil-t-a. t

   , . .              n- s- 7L,               1340             AS          TLI26               73*F \ d,M in-t-x II-l-76 BA-O                             45          TL 125             /n3'F                    NM /n-i-x Il- I-7(> 1340                          46          7C I26               70* C;-                 ANlb. tit-w.

11-I-16 1346 AS TC I27 bd % " LWR m-i-x

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I TEMPERATURE REAulNGS t-' - DATA SHEET 2 PAGE / OF 9 ' TEST DATE TINS PRESSURE LOCATIO.N TEM.= . m m./n m m Es

                           //-/-7L                 l')il              SC.o          TC127             lf *p             &              fli.t. >g\
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-- .. - . :. . - . . . - . . a. : . ~ . . a- _ .a,ww.w,s DATA SHEET 3 PG. 1 0F 5 DATE : 10'/ 31 / 76 f- .
EQUIPMENT HATCH MERIDIONAL STRAINS - PRESSURE 20.00 PSIC TIME,: 22.12 CHAHHEL GAGE STRAIN 480 35M 5.3844E+01 481 35M* 1.7948E+01 482 36M 5.1280E+00 483 36M* -5.1280E+00 484 42M , 1.2807E+04 485 42M* 1.2820E+01 486 43M 5.1280E+00 . 487 43M* 1.5384E+01 486 43M 5.1280E+00 487 43M* 1.'5384E+01 488 44M -1.0256E+01 489 44M* -1.5384E+01 490 45M 2.5050E+04 491 '45H* -7.6920E+00 492 46M . 1.2820E+01 493 46H* -7.6920E+00 (~ 494 495 47 47H* 1.7051E+03 7.6920E+00 496 48M 2.5640E+01 497 48M* -1.7948E+01 484 42M 1.2807E+04 - 485 12M* 1.2820E+01 498 41M 2.3076E+01 499 41M* 7.3774E+05 500 . 40M -8.9740E+01 501 40M* -3.8460E+01 502 39M -7.9484E+01 503 39M* 3.5896E+01 504 38M -9.2304E+01 505 38H* -3.5896E+01 506 37M -3.8460E+01 507 37M* -4.6152E+01 ( . SIGHED E-1 -1. ,
. . - - - .-. - .. u . , m v ,, w w .
DATA SHEET 3 PG. 2 0F 5 , DATE : 10 / 31 / 76 i EQUIPMENT HRTCH HOOP STRAIHS PRESSURE 20.00 PSIG TIME : 22.12 CHAHHEL GAGE STRAIH 508 35H -7.9484E+03 509 35H* -1.5384E+01 510 36H 7.4356E+03 511 36H* 5.1280E+01 512 42H 1.2820E+01 513 42H* 2.5640E+01 514 43H 7.9484E+01
515 43H* 2.0512E+01 514 43H 7.9484E+01 515 43H* 2.0512E+01 516 44H -4.3588E+01 517 44H* -2.5640E+00 518 45H -6.7177E+02 519 45H* -2.8204E+01 520 - 46H -1.2820E+01 521 46H+ -3.0768E+01
/
522 4?H 5.1280E+00 523 47H* 2.5640E+00 524 48H -2.3076E+01 525 48H* 4.1024E+01 512 42H 1.2820E+01 513 42H* 2.5640E+01 526 41H 1.3076E+02 527 41Hu -5.1280E+00 528 40H '
-2.0512E+01 529 '40H* -2.3076E+01 530 39H 2.5640E+01 531 39H* -5.8972E+01 532 38H 1.4461E+04 533 38H* 8.9740E+01 534 37H -1.6922E+02 535 37H* 2.8460E+02 l
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- . - 3 DATA $HEET 3 PG. 3 0F 5 DATE : 10 / 31 / 76 PENETRATION STRAINS - MAIH STEAM LINE PRESSURE 20.00 PSIG TI!!E : 22.12 CHAHHEL GAGE STRAIN 560 76H -1.0332E+02 561 76D -1.2665E+02 562 76M -7.9992E+01 563 77H 5.6661E+01 564 77D . 4.3329E+01 565 77M -5.9994E+01 566 78H -2.3331E+01 -
567 78D -9.9990E+00 568 78M -6.6660E+00 569 79H 7.3326E+01 570 79D 9.9990E+02 571 79H 4.6662E+01 572 80H
-4.6662E+01 573 80D -1.3332E+01 574 ~80M 2.3331E+01 575 81H -2.6664E+01 576 81D -3.3330E+00
(' 577 81M 1.9998E+01 578 82H 1.9998E+01 579 82D 2.3331E+01 580 82M 0.0000E+00 581 83H '
-3.3330E+02 582 83D -3.3330E+02 583 83M -6.6660E+02 584 84H -6.6660E+02 585 84D -6.6660E+02 586 . 84M 3.3330E+02 587 85H ' -3.3330E+02 588 85D -3.3320E+02 589 85M 0.0000E+00 590 86H -6.6660E+02 591 86D -3.3330E+02 592 86M -3.3330E+02 593 87H 0.0000E+00 594 87D 0.0000E+00 595 87M -6.6660E+02 596 -
88H -3.3330E+02 597- 88D 0.0000E+00 598 88t1 0.0000E+00 599 89H -3.3330E+02 600 89D -6.6660E'02 601 89H 0.0000E+00
.(
SIGHED E-3 {\ ..
.. _._ . . . .._...u- n. . _ _ . __ e__. .m _ .. . . . m a . . s_ -,-.._._ PG. 4 0F 5 DATE 10 / 31 / 76 DATA SHEET 3
' PEllETRATION STRAIlls FEEDHATER LINE PRESSURE 20.00 PSIG TIME : 22.12, CHRHilEL GAGE STRAIN 602 90H -6.6660E+02 603 90D -6.6660E+02 604 90M 3.3330E+02 605 91H 0.0000E+00 606 91D 0.0000E+00 607 91M -9.9990E+02 608 92H -3.3330E+02 -
609 92D -6.6660E+02 610 92M -6.6660E+02 611 93H 0.0000E+00 . 612 93D 9.3324E+03 613 93M 0.0000E+00 614 94H -3.3330E+02 94D -1,3332E+01 615 616 94M 6.6660E+00 617 95H 0.0000E+00 618 95D
~~-1.9998E+01~~
('
. 619 95M 0.0000E+00 -3.3330E+02 620 96H 621 96D -6.6660E+02 622 96M -3.3330E+02 623 97H -3.3330E+02 624 97D -3.3330E+02 625 97M -3.3330E+02 626 -
98H 0.0000E+00 627 98D -3.3330E+02 628 98M -6.6660E+02 629 99H 3.3330E+02 630 99D -6.6660E+02 631 99M -3.3330E+02 632 100H 0.0000E+00 633 100D 0.0000E+00 634 100M -3.3330E+02 635 101H -3.3330E+02 636 101D -6.6660E+02 637 101il -3.3330E+02 - 638 102H 3.3330E+02 639 102D -6.6660E+02 640 102M -3.3330E+01 641 103H -3.3330E+02 642 103D 0.0000E+00 643 103M 0.0000E+00
~~> I 4~~
~~SIGHED s ____________________ E-4~~
~~\;-~~
. . _ . . . . _ _ % ' .~:m. - w.. . m. .u m. . u DATE : 10 / 31 / 76 ~UATA SHEET 4 PG. 2 0F 4 RADIAL DISPLACEMENTS
[ PRESSURE 20.00 PSIG TIME : 22.12 CHANNEL GAGE DISPLACEMENT 417 1 1.1426E-02 418 4 3.5696E-02 419 7 6.3327E-02 420 10 2.3800E-02 421 13 4.3027E-03 422 16 -1.6176E-02 423 19 -3.8006E-02 424 22 -3.2196E-02 - 425 25 -4.6264E-02 426 128 -5.2914E-02 427 2 6.1910E-03 428 - 5- 3.6842E-02 429 8 7.0028E-02 430 11 5.5005E-02 431 14 2.4269E-02 432 17 1.9287E-02 r 433 20 -2.9685E-02 ( 434 23 -4.4497E-02 435 26 -4.9303E-02 436 129 3.2825E-02 437 3 7.7418E-03 438 6 2.9133E-02 429 9 6.3910E-02 440 12 5.6250E-02 441 15 2.0355E-02 . 442 . 1S 1.9055E-02 443 21 -1.5883E-03 444 24 -2.0221E-02 445 27 -4.9703E-02 446 130 2.3196E-02
./
~~SIGHED t e~~
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~~3 0F 4 DATE 10 / 31 / 76 DATA SHEET 4 PG.~~
.f- VERTICAL DISPLACEMENTS EQUIPMENT HATCH 20.00 PSIG TIhE : 22.12 PRESSURE GAGE DISPLRCEMENT CHAHHEL 48V- 3.2208E-02 447 -1.5066E-02 448 47V 46V 4.2533E-02 e 449 2.7995E-02 i 450 45V.
~~44V 3.7141E-02~~
! 451 43V -2.5694E-02 452 1.9253E-02 453 35V 36V 1.8987E-02 454 1.6047E 455 42V .
~~41V 1.8038E-02 456 "' 1.8861E . v .~~
'40V 457 1.7470E-02 459 39V 38V 1.6675E-02 v': 9 0.0000E+00 460 37V /. \ . e . . . . .- ..4 - . , g. ;, . ,
~~k 4 SIGHED~~
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~~PG. 4 0F 4' DATE : 10 / 31 / 76 DATA SHEET 4~~
. EQUIPMENT HATCH RADIAL DISPLACEMENTS 20.00 PSI.G TIME : 22.12 PRES $URE GAGE DISPLACENENT CHAHHEL 35 2.9663E-02 461 2.3788E-02 462 36 42 2.6757E-02 463 1.5538E 02 464 43 42 2.6757E-02 463 2.9949E-02 465 41 40 3.9824E-02 466 39 4.7841E-02 467 5.8478E-02 468 ,
~~38 464 43 1.5588E-02 1.6135$-02~~
~^
470 44 . . 471 45 2.1666E-02 472 46 3.0442E-02 473 47 2'.6030E-02 474 48 3.3047E-02
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ML19308D686

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