ML18026A363

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Forwards Suppl Info Requested by Structural Engineering Branch at 810529 Meeting & Subsequent Telcons.Encl Closes Out Action on SER Outstanding Issue 13
ML18026A363
Person / Time
Site: Susquehanna  Talen Energy icon.png
Issue date: 06/03/1981
From: Curtis N
PENNSYLVANIA POWER & LIGHT CO.
To: Schwencer A
Office of Nuclear Reactor Regulation
References
PLA-831, NUDOCS 8106090373
Download: ML18026A363 (52)


Text

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REGIJLATORY INF<<)RHA1'ION 0ISTREBUTION Sl ~ TE% (RIOS)

A ACCESSION NHR:8106090375

>AC.OATE: 81/06/03 NOTAPIZEO:

NO FACIL:50 387 Susquehanna Steam Electr ic Stations

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Licensing Branch OOCKET ¹ 0500 050 SUR.JECT:

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'OTAL 'IURSER OF COPIES REOUIREDt:

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TWO NORTH NINTH STREET, ALLENI'OWN, PA. 18 I 0 I NORMAH W. CIIRTIS Vice President. Engineering 8 Construction-Nuclear 770.5381 June 3,

1981 PHONEr {2 I 5) 770-5 I 5 I I

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C Mr. A. Schwencer, Chief Licensing Branch No

~

2 Division of Licensing U.S. Nuclear Regulatory Commission Washington, D.C.

20555 Docket Nos.

50-387 50-388 SUSQUEHANNA STEAM ELECTRIC STATION SER OUTSTANDIiVG ISSUE 8'13 ER 100450 PILE 841-2 PLA-831

Dear Mr. Schwencer:

Attached are copies of the supplemental information which was requested by the Structural Engineering Branch during a meeting on May 29, 1981 and subsequent telephone conversations.

This information closes our action on SER Outstanding Issue f13.

Very truly yours, N.

W. Curtis Vice President-Engineering and Construction-Nuclear CTC/mks Attachment cc:

R.

M. Stark NRC 373 PENNSYLVANIA POWER 5

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w Ibs/ f'g 7 0 sr=/ 88 Ibm/ jV, S e6'e< +or

$7L gay'. g Ib f~

Bee S'ec*<<

p gg

Ibm, Se e Xeckon 3 9

~2

=

W CL+~) +

w P~

2L 2

28 Nl pqp),gp)

~

2HZ 3 ~3~

Cz) CW)

P~qc +'gn

&cong

/88+ 32 G+ gg 2 5.g. g

/bs.

~2 I~

C<na<< v~ /I'e/y ms.s circe&

+a be uni +e rn

/oc H o~

Vhe b on&

b eon;.

C'h eck Sgr e'ss e s in

/he bon~

b e< rn.

as~. a Ibsf r<.

~/ ~li W

so Cz~~ ~PC< 7s>

/Ig P

/b A.

a.

Z<re zs in Ee b~r:

=

o ooq'78

y. 4.Q

(/2) C8 7s)

II O. 8'4'7 k =

o g~ogo H

//aqua /2 g~, yy)(o F49')C~ 7~)

~oooo x / ~Z I

b.

5'g/-e s in m ~o >~r y

'2

'2 b

~ os Clo) C3 75)

/2ooo

/2 OO CI o a/4l 0

~ 4s5

/. '/y 9 o o/4/

o. s'47 5'2 q'/

2 k p z) Cgg. Wt) j k Co.Z4WCO 4ss) 42)'. g p,si

c. S'oo x I Z3 dk C,

Chec k s heor y

Zz< )c 8'7$

Z

/b s.

bj+

2SG 5 x 4

~ 75

/732

/bs.

N

= j'Z C/wz )C /. zs)

$ 2s@

/&4j.

wr 9/ock wc il-Chec k shear.

92 55 Y. I'Z

/ 9s 2o age g zgooo x/~ 2s' 4.

I P sj

~

Web Area

/7s ~

Cc as~) C4 <<)

/g /5. 5 p gl + /4 580

>c / 2 5 0 k.

DESIGN EXAMPLE H)R CATTERY I BLCICK-V~T 1.

Reference Documents:

1.1 Applicable section of FSAR 3.7b Seismic.c D sign 3<<8 Design of Category I Structures 1.2 3-8.c Concrete Kit bhsonry, Masonry bhterials and ~ity Control Unifona ~>>d~

Code (1976)

Section 20 1.3

~>>ding code requirements for B inforced Concrete (ACI-318-71)

BuQ.din-code requ>> rements for Concrete bhsonry Structures (ACI-531-79) 1.5 Prospect Specifications 8856-C-72 Expansion Anchors 8856-A-2 Concr ete Uni R.sonry 8856~24 'loor Besponse Spectra 1.6 'esign Eras~

8856-C-807 1.7 J.E. Anrhein:

ihinforced bhsonry Engineering Handbook 3rd Edition.

A Published by bhsonry Institute of Am rica 1978.

1.8 Boark

Formulas for Str ss 5 Strain 5th Edition.

2.

Yaterials:

2.1 Concrete hollow blocks H or A shaped we& ultm>> ate compressive

. 2.2 203 2.4 strength f' 1500 ps'nd mor~ Mth f' 2500 psi.

Cells are filled MA concrete grout Wth f'c = 2500 psi.

Concrete fillfor core of double wythe ~s, f'c = 2500 psi.

Reinforcing steel'rade 60; fy = 60 ksi.

Wall ~ckness:

8" Sp

. 10.88 ft.

'nd Conditions: ~ed at, top and bottan - Local and Global Analysis

.Fixed bottom and free top - Story Drift and In-plane Loading Attach~ant:

100 lbs. of vertical load applied at, 8 inches from the face of wall.

Heinforcenent:

$6 8 16" vertical A e 24" horm~ontal.

Symbols and Notatiora:

A = Gross Section Area (in }

A Ter>ion Steel Area, {in )

s 2

A' Ccc;pression S~eel Area (M )

b = width of Ne~r {in.)

c = Distance of the neutral axis of the cracked section fran th extras ccmpression fibers (M.)

d ='Distance be"ween extra ccmpressics fibers and centroid of tension-reinforcement {m.)

d' Dis~ce between extras ccnpression f hers and cen~r" oid of cmoression reinforcement (in.)

E

= Nodulus of riQdity (psi) fm.= S "ess M masonry {psi)

V

= Lowest natural frequency of the s~

(Pw) n F = bd /12000 d~mnsional coefficient used in detemdzntion of resistWg manent of masonry sections 2

.g = Acceleration du to cavity 386.0 in/sec E

~ Moment of inertia of the cracked section (in }

CGRT1 e

I

~ equivalent mxnent.~ inertia (in )

~ yoment of inertia of gross section (in )

.g g ~1-k/3 K = Numerical coefficient deperding on structural lateral force zesisting system k

c/d Y = Story drift or displacement of wall (in.)

D Force corresponding to displacement; Y (lbs.)

s Q = Local bending num nt (in-lb)

M

= Global ben~~

nary (in-lb) n = F ~ = Ratio of Young's nxxiulus of reinforcing steel to Young s m~~us of rrasonry P

= Atmchrent inc~~~~ load a

~ t = 'Ihickness of blochM1 inches P

= As/bd

=, A's/bd 7

= Unit weight (lbs/cuft)

.v = Shearing str ss (psi)

V = Total lateral load or shear at the base (lbs.)

v = Veight per linear foot of ~l M = Tbtal s

. of mll 5.

Freauenc Calculation:

5.1 Frequency of cracked section.

5.1.1 Ncxrant of inertia of cracked section:

Refer to ACE-318-71 Handbook p. 390

c/d ~+ np +

n-1 pi

+ 2 no'+

n-1

~ ./d) (no+jn-13 o')

And

= bd3(c/d)3 +

onbd (d~)2 + (n-l)o'd (cd' 1n our case:

b = 12 inches A

=.33l in s

n ~ 20

= As/bd

.331/12x3.75

=.0074 no =.1471

~ ~

A>

0 (since d'= ~'=0) s k = c/d

,1 71

+ 2

.1471) -.1471 =.415 c = kd =.415x3.75

= 1.56 in

= (.415)3/3 x 12 x 3.753 +.1471 x 12 x 3-75 (3.75 1 56) 2 Z,= 46.94 in4 5.1.2 Eeflection (s&ple beam) weight of t~:

w =

vx b x t = 125 x 7.63/12 x 1 = 79.48 lbs/ft Static deflection 6 static

= 5wl x

J.c~

a static

= 5 x 79.48 x 10.88 x 123 = -35589 in 3

x 1500000 x

-9Q

5.1. 3 Frequency fn ~'

g/A static fn 1

386s f/o35589 5o24 Hz 5F 1'15 fn 6'03 Hz

.85 f-4.46 Hz 6, R~R For acceleration refer to Prospect Specification 8856-G-24 or FSAR Section 3.7b..

O~

ZOIC AL rZSPONS:"

P~

V:"Wjo BZSP e Irzr

=

I w~~.

I DA.'~.

Acc~>

I IFor Y~ Acc I Ift/sec iXG.

Direction ACC" ft/sec s

G.

I I QDK Issv Isa~

ILOCA I

I I QQP Iss~

,Ism ILOCA I

4,5 4.5 4,5 4.5 4.5 4.5 7&

7<+

7+

I 1.25'

.78 g

.03 g negl.

1.40 g 1.13 g

.03 g negl.

EN9-1 FN9-2 E79-3

&9-4 2Z10-1 Fr.a0-2 BE10-3 F&0-4 N/S

.60 g

.63 g

~ 72 g

.40 g

~0-a I FV10-2 I Bva0-3l.

~anal I

I 7.

Local Analysis:

For 1~ of atmd~t (see de~. C-807)

O Cl PRtoo 8LOCK GROUTFD CELL

7.1 Normal load combination.

+

+

o For load canbinations see FSAR table 3-8.8 or 3-8.9 respective+.

t3

= 7.6253 x 1 = 443.32 in4 g

M

= 100 x {8+ 3.81)

= 1181 lbs in g= Mc = 1181 x 3.81

= 10.5 psi < 25 psi O.K.

See reference 3

I33.32 1.2. Table 24-B g

7.2 Vertical Response (Normal/Severe)

Load bination:

D +< + ~ + 4

+ E + SHY +

See Section 'C'f

- FSAR Table 3.8-8 Amplified acceleration

= 1.5 a (1.5)

(E+SRV) = (1.5) (.60 +.72)

= 1.98 g Mt, = '1.98 + 1)

(1CO) (11.81)

= 3519.4 lb.m~

= 293.3 lb.ft

'2 Assam the follow<..(refer to prospect stan"e.rd dra~+w~s C-805/

sh. 1, 2

5, 3 and dra~"~ C-807) 1.

Min. of 2 anchors are used 2.

Min. Spacing

= 6" for anchors T

C (351 9e I/6) 586@ 6 lbs ~

c

=.0074 Men frcm reference 1.7 Table E-15 g =.861 b = 12" d = 3.75" v = (V/gdb) = {586.6)/(12){.861)(3.75)

'= 15. 30 ps<<25 x 1. 3~si O.K.

")

Ref. 1.2 Table 24-3 C

Mhere:

T = M ~wwZe ~~ actmp at the centw liw of kol~a.

C ~ ']he compress've force at the centroid of the compressive block.

Check stress in rebars and In masonry:

(Ref. 1.7 Table E-15)

Z - bd2/12000

= (12) {3.75) /12000 0141 K

M

.2933/.0141

~ 20.80 F

Stress in masonry:

f

~ 2K/gk = '{2)(20.8)/(.861)(.415)

= 116.4 psi

<500 psi m

Ref. 1.2

'Stress in re-bars:

f

= M/P gd = 3519.4/.331x.861x3.75

= 3293.1 psi <24000 psi x 1.33 s

"s For canbination of horizontal and vertical response see global analysis.

8.1 Vertical - loads due to attach~t 8; 'lobal Analysis:

OBE 'Condition {normal/severe)

.OOl'BE

.002 SSE 8.2 8.3 8.4 Y

= 293.3 lbs.ft

{see above local analysis) 0'0 0

0 Horizontal

+

+ > +

+ SRV+ E (E+SiVT) = (1.4+.03)

= 1.43g w = (1.43)(79.48)

= 113.66 lbs/ft (~a~l Inertia load)

P

= (100) (1.43)

= 143 lbs {attac?me~t inertia load) a Story Drift - for displacenents refer to NODE 80 FSAR Fig. 3.7t 58, 59, 6O h 61 00078'BE Y = (.001-.00078)(12)

.00264" D = gp ~/L3 = (3) (1500000){46.94){.00264)/(10.88xl2)3

=.25 lb.

... negligIble Suction of above

+

+

o +

o + SRV' E + Ds M = >L

+PaL/ l+(MZ)(1/2)+{Ds)1/2 for maximum benDIng analysis

( 113 e 66) {10@ 88)

+ {1 f3) (10e 88) (1/4)+(293 o 3) (1/2) + { ~ 25) {10m 88) (1/2)

~ 1681.8+388.

146.65+1.3b

= d4xo.o ~~.i ~

+~ +~ + (~L) { ~) +Ds for maximum shear ana ysis 2

~ (113.66) (10.88) {1/2)+103+(293.3) (1/10.88)

+.25

~ 788.52 lbs Stress in rebar:

M p~~~

Q n

=.0070

$=.861 A ~.331 in f24VAsJd

= (2218.8) (12)/(.331) (-861) (3.75)

~ 24914 psi

< {20000){1.33) O.K. {Ref'. 1.2)

Stress M aasonry:

K = N/P F = bd2/12000 P = 0.0141 K = {2.2188)/.0101

= 157.0 min LK ft]

fm = 2K/Jk

= {2)(157.0)/(.861)(.015)

= 876.8 psi

> 500x1.33

= 665 ps>>

N.Q, (Ref. 1,1)

S&ce the stress in wall has exceeded the towable str ss, a redesi~m of wall, with reduced sp s is reouired.

However, since the purpose of this example is to demonstrate the des~

procedure, such redes~ is not provided.

Shear at N.A.

v V

(788.52)/{12)(.861)(3.75)

Jbb

= 20.35 psi

< 50 x 1.33 ps>>

O.K.

(Ref. 1.1) 8.5 Check of rt~>>

crac FSAR 3.7b.3-1.5)

>>m acccordance with ACl-318 (Refer to

De~ection (03K) 1-46.94 in4 A

. o P

Ao =

5w L

= {5)(113.66)(10.88)

(12)

=.509 ~

3

)

1500000 4

~ 9

)

P =

(K3/48K I) = (143){10.88xl2)3/{48xl500000x46.94)

=,.0942 in QL

{gr.2~Z)(.0642)

{3519.4)(10.88x12)2/{1500000x46.94)x.0642

=.0547 in A

Ie "cr=

Ze =

.509+.0942+.0547

=.6579 in

{acr%) > 'Ll-<<cr'V ~

cr 2fggt; = (50)(403.32)/3.8a

= 5817 81.bs.in

{2218,8)(12)

= 26,625.6 lbs.

>>n (5817.8)3 (443.32)+

1-(5817.8)3,

{46.94)

~2~,(225.8)3

{~((2~.i)3 4.62 + 46.45 3

51.07 in I

Since I I

partial crac~>>

needno+be checked.

ce e~

cr Re&sed

{.6579){46.94)/51.07

.6047 in 9.0 Globa~ Analysis - SSZ Condition (abno~~/extreme) 9.1 Vertical - Loads due to attachment.

1

9.2 93 Ab~~~:.P '5 'P'P /')'

+ 1 5 {P

+ SRV + LCCA).

1+1 5(.63+.50+ ")<

Ref. 1.5 for Value of SRV accl. under SSE corxU.tion)

M',

= (3.3) (100) (U..81)/12 320.8 lb.ft.

L

~ 3897.3 lb.in.

T' C'

3897 lb.in./6 in. = 699.5 lbs.

v'= V'/bgd = 609.5/{12)(.861)(3.75) 16.76 psi < (25)(1.67)

= 41,'p psi Ref.

1..1 Table 3.8-8, 3.8-9 We attachment load will be transferred to the ~all by shear.

Stress in rebar (Due to attadzent only) f

= M'Asgd = (3885.5/.33x.861x3.75) s

= 3657.76 psi

< (60,000)(.9)

Ref. 1.1 Table 3.8-8, 3.8-9

= 50,000 psi Stress in masonry (due to attachment only) h K = N/P =.3238/.0141

=. 22.965 M = K-FZ f

= 2K/gk = (2){22.96)/(.861)(.015)

~

m

= 128.9~'

500 x 1.67 = 835 psi O

Horizontal

+

+

>> +

>> + SHV + 1.25Zo + LCCA (1.25 Eo+SRV+LOCA) = (1.25x1.4+.03+0)g

= 1.78<

w' (79.48)(l.78)

= 141.07 lbs/ft P'

(100)(1.78)

= 178 lbs Story Dr&t (se ~.

A Q. 6)

= (.0012-.00094) {12) =.00312" D'

(~> W')/(L)

= (3){1500000){06.90){.00312)/(10.88x12)

S

"-;296 lbs 0

~ 0 0

p 9.0.

Sumration of above.

+

+ y>> + p- + SRV + 1.25 Eo w<L2/8 + ~~iL/~ + {M'L){1/2 +

D s 1/2)

~r (141. 47) (108)2/8

+ (178) (10.88/4)+ 323.5+

{.296) (10.88) (1/2)

~ 2741 lbs.ft

~ ( >L/2) + 7' M'L + D' (141.47)(10.88)(l/2)

+ 178 +323;8 +.29

~ 769.6 + 178 +29.76 +.29

~ 977.65 lbs v'

(978)/(12x.861x3.75)

~ 25.24 psi < 45 psi Stress In rebar:

s

-.0074 k =.415

~ =.861

~ (M/A'd) = (2741.8x12/.331x.861x3,75) s s

~ 30,777 psi

< 54000 psi O,K.

Str ess in rr)asonvy:

X = N/P = 2741/.0141

= 194.39 A

=.331 f

= 2K/Jk = (2){194.39)/(.415)(.861) m

= 1082.88 psi

> 500 x 1.67 (see Ref. 1.1) 9.5

  • Check for partial cracldz~

~a accordance with ACI-318 {Refer to 3

FSAH 3.7b.3.1.5)

Deflection (SSZ)

I= 46.94 In Z = D'+DF +Q~

=.509(141.47/113.66)

=.634 In.

See page 8 for F="deflection.

0 F'

(.0942)(178/143)

=.117 In.

See ~'e 8 for CBE deflection.

+ g'L =.0547 In.

634 +.117 +.0547

=.8057 in.

I'.~ r%'

I

+ (1 Ncr/N'a)

Icr e

'cr a

2218 83 (.443.32)

+

1 {2218.8)3 46.94 32892

{332392

)

~ 47.06 In = 46.94 in

-1 1-

No further c¹

- for part'ia~ cranny~

~~. t Xn Plane Load

Reference:

Section-3 d~. C-1305 St-8'5'-6" I8'-0" I3'-2't EL.. 789-O 4-O'H)GH OPENING'YP.

EL.77 I'-0" 68(@16 VERT.

ll 44@24HORI ll.

eg ISVERT.

~4@24HORZ T

UNO 5

L = {6.67 + 15.5 + 18 + 16.17 + 13.17)

=

69-51'ssun the fo~~oN~:

1.

Re~~<orcenent

¹6 6 16 vert. (conservative) 2.

Perperdicular mals contribute to load~~

but not to stiffness of wa>> M ~m-plane direction 3.

D flection is less than 1 ]f2" ani therefore ceM~~ structu~~

steel bea.-,z do not suppor t-the s~

{See dra&~ C-805 for ~p deta~~s)

SALL COMPRESSION REINF.

TENSION RE INF.

SECTlONAL PLAN d = (3/4)(L) = (3/4)(69.51)(12)

= 625-59 in d'

{1/4){L) = {31k)(69.51)(12)

" 208-53 in A

= A'< = (27 bars)(.44) 11.88 in2 p

= ~bd

= 11.88/(7.625)(625.6)

-0025 d'/d

333 p

~ A gbd

, 11 88/(7 625)(625 5)

~ 0025 CW P.)

.{n-1) c/d ~

~ (20)(.0025) ~.0

{19)(-0025) "

O475 nP++ ~1 pt

+ 2 n pp n-1 ~pd'/dj - friI +(n 1)

A t'( 05+,Q475)2 + 2( ~ 05+.0475x.333)l

( 05+

.2778

= (.2778)(625.59)

=

173 '

~

I

= bd3(c/d)

+ nn bd {d-c)

+ (n-1)>'d (cM')

Icr =

1 (7.625){625.59)

(.2778) +.05 {625.59)(7.625)x 3

(625.59-173.79)2+(,0475)(7.625)(625.59)(173.79

>> 208.53) 2 34Q, 887. 18+48, 648, 655. 75+273, 453. 12 62,298,996 Not

W above appr<<~" ~or select~

re~or mat and ccmpression r e~~ "orce~t Is approx.

sonly.

An iterative process would be requS.red to locate actual "d" and re~orcenent.

+

A

=wL.

+3'b V~I 5AE Ref. 1.8 page 185 w=bx 7xL w = (.6354)(125){69.51)

= 5520.9 lbs.ft (opens

&eluded)

M = wH-ope~

M = (5520.9)(10.88)

.6354 (4x6.67+4x12.5+7x3.33)125 52,125.69 lb

E Load from Perzendicular Walls.

The loading frcm cross wa11s is added to the wall inert&.

%he

.magnitude of the load depends on spacey of seismic supports (clip

~les) for the cross ~all, stiffness and acceleration of that wall.

En this exaniple nax~ spac~ of clip angles is 4'-0" O.C.

Let U be the added load due to cross wall then:

U

U U3 = Uq = U5 = U6 = U7 where 1 to 7 represent cross wa 1s 1

2 Ul = (L)(

) (b) (a) a = acceleration, see age 4, use maximum

~ value in lieu of calculating freauency for each va.

Ul = (2')(125 pcf) (.635)(1.43)

= 227 lbs/i of heist

.00684 W W = [52126+( Z U~ )j= 52126+(7)(227)(10.88)

69014.3 lb i-I w = 5520.9+(7)(227)

=

7109.9 lbs/ft

> b = wj~

" (7109.9)(10.88)"{12)

.00023 in I!. x ~5t, 9".9~9 a v

>L

= (3) {69410.3)(10.88xl2)

~5AZ(5 (173.79x7.

25

( 00,000)

A static

=.00023+.00680

=.00707 in f

= 1/2 (g/4) 1

1/2 (386.A/.00707) ~

J fn = 37.21 Hz

.85 fn = 31.63 Hz 1.15 fn = 02.79 Hz

. 0

~

Refer to Spec&ication 8856-0-24 for the folio~:

HESPONSE SUYiaRHY z rizontal esponse Peak Uert. Resp l

) LL8 l'T'eO ~

Earp.

Accel.

Accel.

JOE t st lm' LCCA I'

Or~

Is-sls f LCCA I

32 32 32 32 32 32 32 32 7Rqr 7w

.22

.287

.06

.13

~ 21 271

.05

.13 BN9-1 FN9-2 BN9-3 FN9a

.I 0-1 FH.0-2 BEl0-3 PH.0-4 RPT>

~V"~'JP 'EON I

load~ ~~ Co;.>~~~ tion:

{Nor.,M/Severe)

. =--:Szr = (.225+.06)=

.29 g d = B.stance to dooms (very consecutive)

ZH.MT +F~+"+~~+D V = S L (lOO ib)(L/3'

'= (.29)(52126)+(.29)(100x69. 51/3)+{7x227){10.88)

= 15116.5+671.83+17288.3

= 33076.7 lbs 100 lb = a tachnent load per 3 ft. strip as sholem on d~~. C-807 v = V/bJd = 33076.7/(7.625)(.907)(29x12+4)

= 13.58 psi ( 43 psi O.K.

J ~ 1-k 3

= 1 (c/d)/3

= 1.2778

=.go70 3

Yew",e:

By inspection for abnormal/extrene Wvirommtal load ccmb~~tion, in-plane shear is O.K.

/ ace leva*'on spectra per ~~ih'>g

+~ / ~u/cz*dPy Md.

2 4

De a

g ri) 0I-dfKnlI

()

1-C/l

o. 9 r

n Ohr w en 0

0.1 e!

ri n

1O.O 4

6 tt tno FREQUENCY-CPS Fig.&H~ Acceleretion Spectre for hoed Cage:

agegen~ehanna

Node, Direction JLS, Etev Oamping: 0.005, 0.01, 0.02, 0.05 I

dl

O.pl 25 00

~l. 00 z0 K

Wlbio. 75 O0 KI-C.)

0 0.50 U) p

%5

0. 00 O.l 4.

6 8

lP 2

n 6

0 loo 4

6 8

lOO Nede, Direedee~~,

Eiev 749 Damping: 0.07, 0.10, 0.)5, 0.20

>o.o

'.P PEnfOOi 0.1 0.01

l. 50
l. 25 be

~1.00 Ul

'z0I-w D.75 OO p:I-O 0 0.50 U)

~

0. 25 D.DO 0.1 6

8 IP 4

6 0 IPP 6

e IPP I

O IQD A 0

FIELQLIEN( (.CPS Fig.25K& Acceleration Spectra for Load gaze: ~usrtuehanna Node H-S 749'-1"

,Dirsctioo

.EIIv Damping: 0.005, O.Dl, 0.02, 0.05

O.OI

~

l ba dO VI O

~(

Ir.

Idl W()

O I-n.

CII O.I IO 2

~1

" IO.O I:

IOO Fig BEq-1 FREQUENCY-CP" pcceleration spectra ior "E~CTOB R CONTROL BLDrS Laad Care: Muquehanna Hade

.Dirsclion, Elav E-M 749'-1" Damping: 0.005, 0.01, 0.02, 0.05

lp.tr

1. 50 Pf RIOD&c.

tp p.t IiTl~~l 0.01 1

l. 25 co

~1. 00 K0I-K W

w0.75 OO KI-p 0.50 V) 0.25

0. 00 p.t 2

4 0

8 tpp e

S,tpp

& C/I Q 'g O

N g 0

r 8 g 0

LI I

rl

Node, Direction E r:, Elev Dampintl 0.01, 0.10, 0.15, 0.20

ro.ofTl 1 ~ 50 I.p' PEA(DD('JJ O.I o.oa1

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