ML18038A273
| ML18038A273 | |
| Person / Time | |
|---|---|
| Site: | Nine Mile Point  |
| Issue date: | 08/28/1987 |
| From: | Mangan C NIAGARA MOHAWK POWER CORP. |
| To: | NRC OFFICE OF ADMINISTRATION & RESOURCES MANAGEMENT (ARM) |
| References | |
| (NMP2L-1070), NUDOCS 8709030097 | |
| Download: ML18038A273 (457) | |
Text
{{#Wiki_filter:/ REQUL RY INFORMATION DISTR I HUT I 0 SYSTEM ( R IDS ) CAR l
,ACCESSION NBR: 870903009 DOC. DATE: 87/08/28 N t. ZED: NO DOCKET 0 FAG IL: 50-410 Nine Mile Point Nuclear Stations Unit 2i- Niagara Moha 05000410 AUTH. NAME AUTHOR AFFILIATION MANQANi C. V. Niagara Mohawk Power Corp.
RECIP. NAME RECIPIENT AFFILIATION Document Control Branch (Document Control Desk)
SUBJECT:
Forwards canal'g SbW Calculations PX-60012-2I MS-2155-0 5 PX-60160-0 in support of review of final rept on downcomer design r 5 is. DISTRIBUTION CODE: AOOID TITLE: OR COPIES RECEIVED: LTR Submittal: General Distribution 3 ENCL L SIZE: I NOTES: 21 REC IP lENT COP IEB RECIPIENT COPIES ID CODE/NAME LTTR ENCL ID CODE/NAME ., LTTR ENCL PDi-1 L* 1 0 PD1-1 PD 5 5 HAUQHEYI M 1 BENEDICT' 1 INTERNAL ACRB 6 6 ARM/DAF/LFMH 0 NRR/DEBT/ADS 1 1 NRR/DEBT/CEH 1 1' NRR/DEST/MTH 1 1 NRR/DEBT/RSH NRR/DOE*/TSH 1 1 ILRH 1 1 OQC/HDB1 0 EG FILE 01 1 1 RES/DE/EIH 1 EXTERNAL: EGhQ HRUSKE> S 1 1 LPDR 1 1 NRC PDR 1 NBIC 1 TOTAL NUMBER OF COP IEB REQUIRED: LTTR 28 ENCL 25
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V NIAGAR U MOHAWK NIAGARAMOHAWKPOWER CORPORATION/301 PLAINFIELDROAD, SYRACUSE, N.Y. 13212/TELEPHONE (315) 474-1511 August 28, 1987 (NMP2L 1070) U.S. Nuclear Regulatory Commission Attn: Document Control Desk Washington, D.C. 20555 Re: Nine Mile Point Unit 2 Docket No. 50-410 NPF-69 Gentlemen: By letter dated May 15, 1987 (NMP2L-1035), Niagara Mohawk submitted a final report on Downcomer Design Reanalysis for Nine Mile Point Unit 2. In order to complete the review of this report, members of the Nuclear Regulatory Commission staff requested that Niagara Mohawk submit the detailed design calculations which support this reanalysis. Therefore, please find enclosed the following calculations:
- 1. Stone 8I Webster Engineering Corporation Calculation No. PX-60012-2, which supercedes Revision 1 submitted on'anuary 23, 1986.
- 2. Stone & Webster., Engineering Corporation Calculation No. MS-2155-0,
, which'e-evaluates the safety relief valve (SRV),and condensation oscillati'on (C.O.) load definitions and also supplements Calculation No. MS-1869-2 submitted on January 23, 1986.
- 3. Stone 8 Webster'ngineering Corporation Calculation No. PX-60160-0
'(Plant Specific Condensation Oscillation Loads) ~
These three (3) calculations should be reviewed along with Stone 8 Webster Engineering Corporation Calculation Nos. MS-1869-2 and MS-2053-0, submitted to the Nuclear Regulatory Commission on January 23, 1986 (NMP2L-0590). Very truly yours, NIAGARA MOHAWK POWER CORPORATION 87090> 0097'~08>>-~.--- ADOCK 05000+fp PDR,,' C. V. Man n Senior Vice President PEF/pns -3627 G Enclosure xc: Regional Administrator, Region I Mr.,R. A. Capra, Director Ms. M. F. Haughey, Project Manager (2 copies) Mr. W. A. Cook, Resident Inspector
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STATEMENT OP REVIEW CALCULATION mmER l2(77 d9- PX- 600/ 2-This calculation has been revfeved in accordance vith EMAIL-CH&l-and vas found to be adequate. The method of reviev vas: (circle appropriate items)
- a. Comparison vith a similar qalculation (number
- b. Alternate calculation or simplified approach.
- c. Number by number check.
NONINDEP END REV /DATE The statement belov appliea to Nuclear Safet Related gh Category I cal-culations only. This calculation has been INDEPENDENTLY repaved in accordance vith EHAGKH41- and vas found to be adequate. The aathod of reviav vae: (circle appropriate items)
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STONE e WEBSTER ENGINEERING CORPORATION CALCULATION SHEET L 50I0.05 CALCULATION IDENTIFICATIONNUMBER PAGING d.O. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE
- 1) i 7'7 2.R &tD . A'-4cg/2 @v 2. oF 3t
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STONE 8, WEBSTER ENGINEERING CORPORERON CALCULATION SHEET J.Oo/W.O./CALCULATION HO. IIEVISION
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~ 3 1+ WiTH I IlT~ NE2) IN I TR OV T $ 1~ wl zH C STONE B WEBSTER ENGINEERING CORPORATION CALCULATION SHEET 4 5010.55 CALCULATION IDENTIFICATIONNUMBER g.O. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE ~2 12177 E-N x-4, CeI kd I 10 12 13 14 7RM LC-=, iAi&iIamb R~k. 15 16 17 18 22 24 ~ 27 28 29 30 31 34 35 40 41 42 43 44 45 46 'll W el k+g '~1lt STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. DIVISION 6 GROUP C44,CULATION NO. OPTIONAL TASK CODE PAGE~~ I2 a0 t= lNO Y~-0e u x oF Wua~ CiiYe W Sd~ ~ ~~M i+ s~ d~ i') ~ ~~~ c~ d,/f~ ~,6 i~ 1~$ (, g ~ P. 2>A pa~+~ ~~8 74 Qk 74 A~ ~. 4~ ~ s o6/~~ is M~4;P tI tI sU) i. ~~ e ptk o4 J ~ shing g-jhow t. 4s gyp cled tk ~. ~A o] QJ dms (K ~ g r)gnip~A- ~ Mc Aha t4 Q Q Q > Q Ol Q > + + lO + 0 y + us tO 0 IA e 0 Ulg y y 4 y N 0 O CO lO 4 y y lO lO os lO PO yy t4 0 '4 + 9 8 o 4 8 + 0 0 0 V 0 g 4 EJ IO IA6I f Qo SWK 9 0 P. SSFie l.&iMs pAO t- lac ti 8 NO Mo H ('Ih rill,ggr YA5 3)EFceeTI& QO~ f- L'i)I ~ p'fuhc 6>> j(g pa>~7; F=a;k ( L~fiI FLUID g~Pyg X, >C'/OKER Pm+ ~Cfog = r') K. V I A 0 m 2220 Cl 3o Ig O I O Pl PIP/ C '0 o ~ l I ~ m sf'/ D O l O cn ~OA m 2)29 >>": l o3Il.$ 2.II22 + CA iE o m K ~m C) Skat I go x 0 m 93RV ~~ 0 A Z m ) CO O O 2./ 2592 :l.oM Sl9f M1 2(k7 O R CO m Pl g> O Ao O O I a%Ha I z o O O m p "Sp 'I % ~ I Og I +V ) STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET 4 5010.rm CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE >@ lares <~O PX aW bv . CF St Su~hr A4 OF PCS ur.7 Fr% Fll.m sE cfire .s: 5 II 4~ V 2D 6 4 SI4i< ylh>IZ~ ~~ax~ kYPa4d'~e <~ S'CV e <+~ tuAIC 10 IS 70 gc crwgr ng r Nr %le FAur-Tep k cAsr.= Lm crsrgrNrrlr'aJ rrr ~. 2O (If, w)Ta Cok ssc) ~0 lg <IP O~<<~~<< = 2. S 16 g~7 A7 Fi<v my - )ggQ. 8 kIP- IA Ie 19 51Pesy P ZCSI 20 21 23 24 23 26 22 26 29 30 31 32 33 34 39 40 4$ 46 ~ <c q.g<< Tf; (b,J pt tt STONE 8 WEBSTER ENGINEERING CORPORATION CA LCULATI ON S HE ET J.O./W.O./CALCULATION NO. It EVIS I ON PASE lCHOO/ 45010 61 l 217,0g F' P lt K PARER /0 ATE ItEVI It HKCNER /OATE INDE)ENCE T RKVIKWKIt/CATE Vlzly CHAMPS ~88u6"I57 ~ c /-'rU8 JECT/ TITLE OA CATKSO RY / COOK CL ASS .oo~eeyn>zg gzsporv~s 7-c Zp(! AIRBU88t E LoM CF ~ ~ 3 l '7. NQLUG IC'N 9~% E&rneF~R7ldhlB: 7 HE E F f~ N7 F L Ul ~ ~W')PIN<p /S 5'/C)/tl/F/CPr'1 /Iv 7 /f 05 8 Qf)ZE 5 HH F7P< ~7/I vc 7UPE YB-0cl79 /8 Qg/7E'f/64 ~) j MFS. 7d FLUID u'E2 d </~J. t legs ply cv~~ r~1Lys'iz c~ s~ oo-er ~J gEPP,F~~,7ovg gpE Do~re C~FP~ //6 6 8 us>I DEz~ 3'Ez W F gEz-D~ g//~p) L E 3F Cpg~ ~ F']PZ~~~ 8~)L J </5 /'C7PFc~wz D 7nz-N 0 8vv8 p7 nous T 8E sp c'its'& Th/7 Thr Sg~7M re.~ 7 o PAL f g~g~up /~~ /~ /fan dC/7/CK Qd md 7 , Ch &v g~. /4 Th'F IVF~~J7 WMlL-gr1~ pnJLr /= P/=g uE Mg'd fl 5 047 8/(ED +UP TffF F~ I/'ciao c/7J ~ 8 8/NC)L E Q. d. It. Sr 5 T~ (~ ~ I DEgl 8t.J~ ///p)//~ 7 ffttw'EH~ v FLcrci 7+ ~ ~pF Zug<C gC>'~ /'~T ///= Du~a ~am~ 8g Do/nt c; Te/S 7'//zUXe crt, .. Q~ 8E 8vo(8~ ~M z//~F ~znPv8,7ls g nlic'//7 /Iz g~c vz8, 4~ 'th; ~ 5 tl 1~a 4. N g' 3 f < ~ STONE S WEBSTER ENGINEERING CORPORATION CA LCULATION SHEET J.O./W.O. /CALCULATION NO. t REVISION PAOQ 3i @5010.81 l2177 o8-PX- 6'Do/Z Od 25 PRKPARKR/DATE REVIKWK /CHECKER /OAT INDE KNO N ~RVIKWKR/DATE III'I/WnrDRA 26 ZuI- ~ 1979 ~ yC /'A SUb4ECT/ TITLK CATEQORY/ ODE CLASS PO+NCyhIZP PESPONtSZ TO SA'lI Hlg BI/'88LE Co88 Q/ SZ) I
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lg 'I I ~ lV ll el <v 1 PAGE ENGINEERIHG HECHANICS DIVISION COHPUTER LOG (CAN <<<<<<<<<<<<<<<<<<<<<<<<<<1 CALIIEAIICHNEHERi g P)( GCglk 1 EAH CCHP. AHTHA if'( CHARAC hlASER: was OTHER: LI8RARY JOS FICHE LOC PREPARED 8Y: CNIP UTER CO1NIENTS REF. VERSION Rmt SLSHITTAL USED tCRSER 4'EVEL to. tNHSER SECT PAGE DATE OTHER PERTINENT INFORHATION cs~P 3oZ>>>> gWRC -li'gw a cssP 2 l~ g gelt:c unt W v do M b-l csee 3 $ 033 gag I d4eE << = COt1PUTER GEHERATEO JOB SU-HITTAL NNSER $ k>t'bg/u/gg g01VQ C)l'gC'KZ~> 3'f <<<< -" C01IPUTER USED tSHEC OR OTHER) <<a<< > IF OTHER THAN SHEC CO11PUTER IS USED UMBER LOG f,)oA RUN CALCULATIONNO. ~17< tP'~>> &V2 JOB ORDER NO. 7728 Fl" ATS NAME DISK OUTPUT TAPE CPU PROGRAM JOB DATE OUTPUT (I) TIME DESCRIPTION CHE NAME NO. INPUT (I) OUTPUT (I) NAME NUMBER (2) NAME (MIN) (3) 3 K76 II, P.= ~/~tP -XgdF )fog. ~'SH$ CSHP s) K rc S2. f.':.kP Q~P oi gz Y cMl - Her ttny~g. n n Q I (I) CHECK WHEN DESTROYED (3) PLACE YWHEN GENERATED AND+ WHEN FILED OR DISPOSED OF (4) C NUMBER APPEARING ON JOB CARD (RYYYYC~XX ) (2) CHECK WHEN RELEASED 1AWI1 I I\ W \ ~ ~ l STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET 4 5010.5$ CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. lgl<7 ~ DIVISION O'ROUP CALCULATION NO. PX- 600/ OPTIONAL TASK CODE /I VI, PAGE (f'f'/I&IICM 7 IO en+/orsk P~ l2 l3 F/~7/& I4 l6 17 18 l9 20 2I 23 24 2S 27 29 30 3I 32 33 34 38 39 40 <2 44 18 ef ~ 'C CT '5 eQ A ~% ~A ~ 141 q>p s 4A t 4' '0 at
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//SRV EXEC CSHPX //X.FT06F001 DD SYSOUT<A //X.SYSIN DD %, TITLE NHU-GE HYBRID HITH FSI{ SRV LOAD ON DNCNIER FUNCTION PIQO=(0.0>>0 ~ 0) ~ ~ (0.144 ~ 0.0 ) ~ (0.153 ~ 0.0 ) ~ (0.ides 0.0 )st0.171>> 0.90) ~ . ~ . (0.180>> 3.80) s(0.189 ~ d.00) ~ (0 ~ 19S>> 4.90) ~ 0 20.~ 3 60)>> ~ ~ ~ {0-2lds 3.10) s(0.225>> 4.10) s(0.234>> 4.30)>> 0.243 R,40)>> ~ ~ . (0 '52>> 1.80) ~ (0 'dls -'3.10) (0.270>> ~ ~ .'O.R79 3.80) ~ I ~ OI>>ss ~ ~ (0.288>> 4.00)>>(0.297>> 13.10)s(0.30ds 27 30) ~ (0.315>> 30.6>>s)- .. (0.324 'd.90) ~ (0.333 'S.50) ~ (0.34R>> 10 ~ 00)>>(0 351 ~ 4 79)1 ~ ~ (0.360>> -2.10)s(0.369>> -4.90)s(0.378>> 7.90)>>(0.3Sl>>- 11.0v) s. l 0.39d>>-12.10) ~ (0.405>>-13 ~ 00) ~ {0.414 ~ 13.10 )st0.423>>- 12.40)>> ~ ~ ~ l 0.432>>-11.80) ~ t 0.441 ~ -11.90) ~ t 0.450 ~ ll.d0 ) s(0.459 ~- 11.40) ~ (0.46S>>-10 90) ~ (0.477 ~ -9.70) ~ {0.48ds -8.10 )s(0.495>> -d.dO)>> (0.504>> -5.00) ~ (0.513 ~ -'3.30) st 0.522 ~ -1.10 )>>(0.531>> 0 00)>> ~ ~ F (0.540 '.30)s(0.549 ' 00) ~ {0.558>> 2.00 )>>{0.5dls R.oa). . t0.576 '.30) ~ {0.585>> F 2-50) ~ {0.594>> (0 dies R.dO) ~ (O.d21>> R.10)s(O.d30>> 3.10 l ~ (O.d03 ~ e.50).... 1.90 ) <<(0.439>> 1.10) ~ ~ ~ ~ (O.d4S>> 1.30) s(0.657>> 0.9u) ~ (0.666>> 1.00 ) ~ (O.d75>> 0.00)>> ~ o tO.d84 ~ -0.20) s(0.d93 ~ 1.00) ~ {0.702>> -0.80 )s(0.711>> -1.10) s... ( 0. 720 ~ -0.70 ) ~ ( 0. 7R9 ~ -0.90 ) ~ ( 0 ~ 73S ~ 1.20 ) ~ {0~ 747 ~ -0.70)s.. (0.756 ~ 0.00) s(0 ~ ld5>> 1.80) ~ (0.774 ~ 2.90 )>>(0.783>> 3.20 )~ . ~ ~ (0.792>> 4.10) s(0.801>> 4.I60) s(0.810>> 4.60 ) ~ {0.819 ~ R.90)s... (O.SRS>> 2.40: >>(0.837>> R.10) s(0.84ds 1.20 ) ~ (0.855 0.70) ~ ~ ~ ~ (0.8d4 1.10) ~ (O.S73>> 1.00) ~ {0.882 ~ ) ~ (0.891 ~'.80 0.00)>> {0 900>> -0.30) ~ t 0 909 ~ 0.10) ~ (0.918 ~ ~ 0.30 ) ~ {0-927>> 0.80) ~ ~ ~ . t 0.936 ~ 1.10) st 0.945>> 0.80)>>t 0.954 ~ 0.40 ) ~ (0.9d3 ~ 1.00)>> ~ ~ ~ (0.97R>> 1.10) st 0.981>> 1.10) ~ ({I.990~ 1.70 )s(0.999>> 1 ~ 80) ~ ~ ~ tl.OOS, 2.00).tl.oil. 1.90)>>t1.026. 1.50 )sll 035>> 0.90) ~ ~ ~ (1.044>> 0.00) ~ l 1 053 ~ -0 ~ 70) ~ (1.062>> -1.40 ) s ( l. 071 ~ -2+00) ~ ~ ~ ( 1. 0 SO ~ -R. 50 ) ~ ( 1 OS9>> -3. 00 )>> ( 1. 09S s -3.10 )s(1.107 ~ I sIO)>> ~ ~ ~ ~ (1.116>> -2.90)>>(1.125>> -2.00)s{1-134>> -0. 70 l s t 1.143>> 2.90)>> ~ ~ ~ t1.152>> 4.10)>>(l.ldls 3.30) s(1.170>> 2.40 ls(1.179>> 1.50)s... t 1. 188 ~ 0.90 ) ~ ( 1. 197 s '. 0 ~ 70 ) ~ t 206 ~ 0.50 )s(1.215>> 1 dO)s ~ ~ ~ (1.224 ~ 2.80) ~ (1.R33>> 2 ~ 00) ~ {li242~ 1.10 )s(I.R51>> 2.50)>> ~ ~ ~ {1.260>> 2.00)s(l.Rd9>> 2.00)>>(1.278>> R 10 )>>(1.287>> 2 30)>> ~ ~ ~ (1.29ds R.80) s(1.305>> R.90) s(1.314>> R.RO )s(1.3R3>> 1.80)>> ~ ~ {1.332>> 1.10)s(1.341>> 1.20)st1.350>> 0.70 )s(1.359>> 1.00) ~ (1.3dS>> 0 10) ~ (1.377 ~ 0 70) t1.38ds~ 0.70 )s{1.395 ~ 1.00) ~ .. ~ l 1.404, 0.00), t 1.413 ~ 0.40), t 1.422, -1.00 )s{1.431>> 0.90)>> ~ ~ (1.440>> 0.90)>>(1.449 ~ 1.40) ~ (1.45S>> 1.00 )s{1.4dl ~ 0 00) ~ ~ ~ ~ l 1.476>> 1.00) ~ t 1.485 ~ 0.00) ~ t 1.494>> 0.30 )s(1.503>> 0.40)>> ~ (1.512>> -0.70) ~ t1.521>> 0.30) s{1.530>> -0.40 ) s(1.539>> -0.90)s tl.548>> 1.20) ~ {1.557>> ".1.90)s{1.566>> -2.10 ) st1.575>> 2 50)) ~ ~ (1.584 -4.00) s{1.593 ~ -R.80) st 1.dLR ~ -R.dO )sll.dlls -3.70)>> (l,d20 ~ -d.50) ~ l 1.629 ~ 8.00) ~ l 1.63oI ~ -8.90 ),(1.647, -6.00)>>o ~ {1.656 ~ -5 50) ~ t1.4d5>> -4.90) ~ ll.d74 ~ -3.90 )>>(l.d83 ~ 3.40) ~ ~ ll.d92 ~ -F 00) ~ {1.700 ' F 00) ~ {3 F 000 0.00 ) ALP=(0.0>>.83>>1.0) 'ARAIIETER CONSTANT K=12867.>> H=86.78, DAIIP=1.0>> CD=0.7>>... RHOL=1.94>> A=1.O ~ L=ll.O INITIAL C"-0. 02<<DAHP%t K%H)%>>>>0.5 INCON RZ=5.0 ~ ROZ=O F 0 'DZ=O F 0 'Z=O ~ 0 O'YNAHIC P=AFGEN(PHHU>> TIHE) PSIIPI¹45.33>>>>P t~ j 0 IH/RHOL-1.5<<RD<<<<2)/R Rb-,.sGRL(ROZsROO) R =INTGRL( RZ s RD ) PROCEDURE AVACCsAWEL = AA(RsRDsRODsLsA) AWEL=2.<<R<<<<2<<RO<<( . (-.5) 1/(ReA)<<<<2 (littL/(RtA) ) <<<<2) <<<<c -.5)-t l.i(2.<<L/(RtA))>><<2) <<<<. AVACC<<(R<<<<2<<RODt2.<<R<<RD<<<<2)/(2.<<(RsA)<<<<2) IF tTIHE .GT, 1 ~ 7) AVVEL=O. IF (TI)IE eGT~ I~7) saVACC <<Oi ENDPROCEOURE XOO<<(l.l<<3.14<<2.3<<A<<hs'"..NOL<<AVACC + CO<<A>>L<<RHA.'<<(1 i~<<VEL-ALP<<XO)<<. ABS( 1 ~ 1<<AVVE =ALP<<XO)-HssX-C<<XO)/H XO=INTGRL(XOZsXO(s s X=INTGRL(XZ s XO ) Vl(XD=AWEL XD PRINT XsXDsXODsRsRPsRODsPsAWELsAVACC TIHER FINTIH=2.7 ~ PRDEL=.100s OUTDEL<<009 RANGE XsXDsXODsRsR()sRODsPsAWELsAVACCsVHXD TERHIHAL ENO -. STOP /<< // ~ my ~if Ilk 1 Il STONE B WEBSTER ENGINEERING CORPORATION CALCULATION SHEET L SOI0.55 CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE ~~ )g) p o~g. ~/4'Rc)M~ /M j'w~x~ zg ~4'~~ ~~ 7flF ~~~( 10 rh.&4%'af'uipP w+F l+a 8 o>~fan 4y w~~c am~~roM ~ pc ~aural WR m~4( ~u<Trohf 12 13 14 (f/~> Jy ~ -I.a~g +ay @A<4 aryan~ C6 ~>> A~XWa /f/~alia.~~X'+ p 15 16 /~ b'd d'6:QS 18 ~Aug ~ /a //', c ~l 19 C'CP ~ +r7 c o oJ T sw(0 le Cklfp/) (l /9 Pg 20 21 22 23 ~ a,+3 Cw~w~ ~yJ 24 ~ <i~/OP 25 26 )ep ~ -8 a~ RT HWPC6 4 d'S'Sip 28 WV~ > fAf ~f 29 ~u~i//~ ~ efv VMS rm~ ~oM Mvg~arV, Pr Z~ 31 r8/xZ,f/'~,aX f,a rc//efp'p'~C~./Per)r'p>>/x ff ~ /f1 + /rg< a, df'6g-"O, pg q /-g,~pry//r f/W ~ dpi/ - d/ Pg VC-g~rj />dp4l'- ~ ~loll ~giaspw r s~Jg/arp'-y Revag ~~ ~ ~, gP R. 40 4 Mince Wyatt eve Jacet acsc cz'Mu~w Aa4c z ~ ~gee+ gm~~ 41 42 44 45 46 >A 'l I > t g' 4 ~ ~s a~S STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET L 5010.55 ~ CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE uI~ SN9 Yy- C,oo l k1NMzeAf g U~ie IO l2 l3 l5 l6 18 l9 20 2I 22 25 28 29 30 3I 32 33 34 35 38 39 40 4I jl ~ IA l 4 t4 illc %4m ))( ir STONE Ec WEBSTER ENGINEERING CORPQRATION CALCULATION DISTR I SUTION LIST PROJECT NAME CALCULATIOH TITLE4 +<o<~f~~SE To S 8UggLE'd~(f 5'.zg J.OP W.OP CALCULATIONS REVISION% ~ pP~~azooz~ PREPARING GROUP SUPERVISOR /LEAD ENGINEER NAME 7 . Chn& A LUONg. LOCATION ~/wdi GROUP/PROJ ECT ES F NS N OISTRIbUTION bY OFF-PROJECT STAFF GROUP DISTRlbUTION bY PROJECT NAME LOCATION GROUP/PROJECT NAME LOCATION GROUP/PROJECT '3 P/ PE s7gF'$$ Cat Cg s7-~F (AM/ 8mW6'~ QCj ny ~~llgZ. S7P7 C ~ C.S.LAX ps'/get PB. f'ccords Q+~ EM g'.3 i~ 5Y 4 f>> 9)i; ~ w I, '7r g1) GE I OF +g j/zsid~d>- giga . ~pc/-0 STONE 8 'INEBSTER ENGINEERING CORPORATION ENGINEERING MECHANICS DIVISION PIP~ ~Tv<<~ <<~F F SECTION NI hC>~5 tne&iHvK + I+i CLIENT I OCATION N JOB NO. CALCULATION NO. I~i7~' REV ~ TITLF EGfhJ hl C4 8 g EStFdhJSe To ~ ty HrR SO88~+ Lo~ C F S. ~.) EQUIPMENT/SYSTEM CODK CLASS NUCLEAR SAFETY RELATED YES gl. NO Cl QA CATEGORY PREPARED BY ~i ~t BATE 03 HVAR'i~~9 REVIKWED BY DATE ON-IND ENDENT -- REVIEWED BY TF/ ./P/J/ATE - '-'/2.=:: INDKPEN ENT APPROVED BY DATE i~<<< TITLK CALC. STATUS: 5 PRELI MINARY Pl, FINAL P~v X Q.cVX Aj sf 'I4vtle > t) 4 't i) l pa" '),' fvP lt STONE E WEBSTER ENGINEERING CORPORATION CA LCULATION S HEET J.O./W.O. /CALCULATION NO. IZ/77 d8- PX- fC'0/2 -) REVISION dd PASE PREPARER/SATE NEVI K / KCRKR / ATK INOKPK 0 jNT REVIEWER OAT! p~ /2 i V Z/I epp<D/'/I ~ZuL 1~79 / or'>< s ~ r SUS JKCT/ TITLE OA CATESORT COOK CLASS )o'htN5'wEf A'Est'dwss 7'c'S V tI(R MII~<<~tID Ct' ~3 7//E7/PF/IJE'SZ dF ~(/IJC)LE DEC)AEE gf FgEEDdng ZJS TEQ I/IIAS DEFI E 7E g~ a+ / IP ~ISP~RCEJ9ENT.. Co F E D ping/5 8 Q AS Pd~CE N+ 5'/A/gfQ S S TEA but7Wd7 FLUE D&~PZNtg. ~ /llgL 7/ OEc)/EZ T//E E IIJ8LFrVCE 8E 7WEE~ -'IW>LE Harb / ju/ TiD~Cif'FZ O7 SPY PIPgFLS ~I TPOII 7 FLuiD @CION De PI nICj HAS />ZZ N E STttIQLI ~HLQ. 7 ~ Lode)S C'QLCdL 8'T~ tN E1$ wFIPF UKE/3 Fdg,7HESF 7>o C"r>SCS. IO VER)FP THE VALIDI7g ~F TnE NETVoO PI'E<~~ED IM TI-I) 5 cf)L,evLij tlofJ THE Cd' FIBBED 6'7gc65 ItJfl ~ 4L S6 CI)LC UL 8 TEl0 4l THOUT FL DID QAmPln'C) USt NC~ Nt= TMoD. Fa LL,cwr NC~ g~c f ~g ST PE'~E', < QovC Ttt PC E CA S<$ hl I THOU7 FLUID OHtrlPI NCy /I/ D /NCLUDINCj Th'; I/XM~D'in~/<< ~/'I ~S EO7 ~ 0< UD/N C) 7ffE W/jS~ df Tff Q At /I 7~ k'4) U gE'7 HOLI LO/lj) W(TP lq ULT I P. g, P. Kl 7tll//'~Q 84~/It ~~F78 = 2. I 8 gS g I 7g ~ k u me~II09 Lc AO w~~q Sl~t."Le r.O.F. = ~ k~l I 7) PR<a~T NET o 9 Wl'Tp Gl g 5 Do F; 22 S t ~I. T III~ N UN8 ~RS CZTHIN EG 8 5 Fd LLd ~S: FR~ f93, THE P~ DIZPLRcG II~ IS o $ 3 I 4f, pE STtFf~ss IS II26 Q LpF /gt'.73 sea'o~N crniFp L~c~Tn =. Qs.688+8. C't3 r ;. FI XED Z~ rqOem/T = /I24$ +O S'9(w 45'C>9 ~SF'i'. Zsc7t~ rncmu.r.us = /g p 5'TILE~ = 22 S p -k'S.z. 'i".'f j, VW ~ ~ ~ N t ~ III O gc 8 7 ML d. Im u )OAT Q o c I O I To TAL STIF F.- STRucvuRlle Flxh]o a ~ O Cg Sp gv. EF F E'C1IVt NESS DbrnPINrj V g cv1 Vsp V~~ Sgt <ION R (~) NIQ S5~(wqmg K c~g (p~ ) Vst, me PuLuS, g SI.uC>) gg (L.GF gt-.) (A/&ng C+l~- ) <t) ~~j tf R. ~ ~ I J. y'0 . o nze9 s d37 1 n73 B3 a 7(g o 093y / 937' ~ tg 74.o (/2 df /Iffy '7 5' I QQR 7$ '2 o o93$ / 9a76 //8 0 (IZ dg 2.A 7 3-66lg Q n.722 ~ ~937 / DQp 0) (< I 8I ~ (Q /os~~ 4.]7l 5 SM,o~l y. '7/$ o I$ 0$ 2 /s'4 0 m 2 ip ~O Hl Ig (ABSO 3 905 5 593IS o (P~q X m IP 73'ls OI nC' w' I ~ ~ i I.2 s 'l6 g 8'9o 9 4'29 Q (o5'0 (HE o p 17so6 ga Ill L) o X R m + ~E' p)fl I gE X 3 ~Fdg DEs ~R')O'TION fv D Q 0 0 0 z 0 4 yr Jf4 is ,1 l. 'pl STONE K WEBSTER ENGINEERING CORPORATION 4.0./W.O./CALCULATIOII IIO. III 0 II PAIK 45010.61 thERARKR/DATE /2/7 7' 3 Px-WK /CHECKER 6yo /2.- RE V VIEWER/PATE RK /PAT INO~PK 0 $T h PI~ f /P/'I >-f P <77 /H/Cy /97/ BUBBLED I SUII4ECT/ TITLK 4A CATEOORY/COOK CLASS , gO~ue<~ gas PO~S C 7-O S'RII@R ~4) H'<.~.) I E .~UL T 5: 7//C SO< u T/ONS oF Ep ug T/0 A'I./ ll~/O gC'gag'ts c/I //S M /Al SEC'/dN 6 9. T///= ~ mN 6'nl TIE PEP% DEFLFi'rim A4 I-I~~ E~ P~yt- g /e~Sg ~/Th'N ~/Vy~u7 /=ZO/8 D8riPi/IJ8 uF/~'~W/Z~ /> 788/:e 2 O~ PR6'E 2./o:. jffI- P~ ~ I 7/~ IS STIFLES g)Zf C5'/9/~ / Ad% THE Qg p7 pd7 zX. ~7 /07 . 7 RE IMfs7PF ~~ Is AMR7~ /0 I /gE$ WW ~y ram Fo~L04/ Ald FcQ NUL 1, Z/W~~W ~TlFS~ = THE'IXM t=hrD p~ STR'EBS lS l4vT NE'EssRRlt y l-pE. HID)'t(F ST Q'T gCSS '1-M S Vl F:Fs'fPl3 DO4JNCdtrl 8ygE~Sc~ hhvE gg:-4 C~LCu/RTW TO Psalm 7eF ~, /h'+ EFFm> O7= F'Z u/D D~PIrV Cq, JEST ~i~C< C73 8 / iUoL 7) 8/:- I/ S M F os >E T8// EG <TA ~< RE l'&T 8S EW PF C 7ED THE 9 7'/ 'ZZ' OF F < L/ID 6+ Pl hl +) /5 ~IGNI F) C+7 0/V/ J NIHIL.hl T ff E' TII'I/$7 Ul+ V&P( I 7g <(CNI t-( <&~(L> ff t (i /l~ 'T<+4 FL U<Q 9 E Qg gl 'Tg 'TH~ H)C)tt t: 5 T g.A~ c 7/0< (N ~ 7RL >5 tv/) s <r8itIi~m iN c./IsE f b rc> is 4 79 4Sj:. g ILAW ~ Ill+ lpbg ~ I' 1 I 4 7" at> ~ VcO c 8 788 L E ~ C n C Pa rO SIXE"LE 0, g.. OqFLet'WI ON . AAJ X) FIXED P nrO S TgEwS ~ zq ~N I g O FILLED STRV Cavfl STlf'FF uED W I '7 HOVT f LV IQ Wl fH FLUID O R sE 'R C'A 0~PI NCj D PIN (my~) K. Wo. F NI PTy (W: HSTlFFEN~ P~ FIXE D IE Al( F'glCED Dew u CutntR Ilgwu hl lIl+ DEF L E CTin Q NT) DFFLFcTtoN EN0 F= FILLED S< STIFF, (v~> STReSS (gy. ) STgF S5 (S'L OC~) g Gf /Pg C = E lnPTJ< U= VH~Tlfr (xs~ ) 0 0'$5IOI9$ 2z sg o $ 6Ss CsJ /7 7Z 74.a ) i'24) I ~~7~ ~C '2 s.nD j l9'9 5 $ 37/tan l(o'4/ 74 6 II 2.6$ I 9374 ZDrb O 0Z W4 A 0 0346aM /3'~'3 035I IQ< j3 +I ll8 9 CIRCE l ~'t3 I X m ID 1 Vl m d~ASS9Q3 II I QP ~ QlyBpi / 7g 8I lg l489a 2)S 0 I I m Z C) 0 O Z 5 o 4I78033 lo 9Q 99~ O~> /~ 't7 Bl IQ (489o ~X m m 2 .I Z S 't29QIf 3858 DB /o /0 l>$ 'IF IQBBO l 75' C) O 0 4 0 Z 4l O Cl ( O I I ) ',I I'I I I I Cp y4 I COMPUTER LOG I SSW AUTH. NO. 0 / F5 PC TION NO. IZ(77 o$ '-Px-Spoil 7729 COC CHARGE NO. JO ORD RNO. /~/7~~ ee ~B NO. FICHE LOC. PREPARED BY REVIEWED BY COMMENTS SECT SIGNATURE DATE S T DATE loves <6hv4 AO CC. ujW Dary Pi jd g CJ go7O (ev9 25'3u~y C'p- d'3 ~ lyr s'Tif'. DAePjN O'S /-~C. d $ /Pp D~~ 4'OOPT d'6 R I~79 < ~/fs/y ~PTg D~~g.if o a./)AC> Cg-"d TGscu4$ sly. k-"II%4'ylg C4gP go7os = C28 /w7 o~]p. any go?'/f 05Pjg g Q-"r, ny ~ p/ /ps ~ e P /079 /~N k IQSSdMr/Ir'. oj/ r=/,z 5 go70r 66 Hog ~0 +j R - /<5'I f << u<j I e8y PYB = A 8 ~d id~/'A'e- r = / Q=d 7, i d OmP Z:Pg gl70f op Iq79 Cg WEB f =(!2,8 0 /at.P-"o 7lg C 72 2- $~70S I goal //d /9'7P ~ < giuf c>=< z (qo, N
- C gp..AP=d 4'-/jVSq 7< ~
Iron Cl S fo7//f o p'A4 7W Ng n d j in= Jvo = /4/J+<</a, a/. o.>> P1 = /2 9'/ $ pg,l loI ]$ 79 "iv/p S$ e ~< 8 soLp p,4p-o.>~p Cu=d.7. o &= 9/ I4 07 '9 i - (g Se~C8r/P, +/.d-498 os'A6'97 Cij= o y. > o, A '7< Cb/ P K-//~ay Mjjg~p.p-.ygZ + COMPUTER GENERATED JOB NUMBER +,+ coMpuTER USED (saw oR coc) 4 fit" A Sk H l 'V4 lt, pl 3 J4" I+11 " 'Pt Ol 4 Qp //R0745Cdl J08 CHtV.CHAHDRA. >HSGLEVEL=l /t>>J08INFO R=230K> T=l>>PHONE 3734 //CS)IP3 EXEC CSHPX //X,COHPRINT OD OU)0(Y>OISP=(NEH>DELETE) //X>SYSPRINT OD OLROIY>DISP=(NEW>DELETE) TITLE KHU<<GE HYBRID HITH FSI) LOAD ON DOHNCOHER FUNCTION PKHU=t 0.0 >0.0)>> (0 ~ 144>> 0 0 ) ~ (0.153 ~ 0.0 )>>(O.ldZ ~ 0.0 ) ~ (0.171> 0.90) ~ (Oel80t 3e80) ~ (Oel89>> 6e00)>(0el98 ~ 4e90)>>(0e207 ~ 3.dO)>> ~ .. (0.216 ~ 3.10) ~ (0.225>> 4.10) >(0.234>> 4.30) ~ (0.243>> 2.40)>>... (0e252 ~ 1 80) ~ (0 261>> -3 10) ~ t 0 ~ 270 ~ -3 80) ~ (0 279> -1 00) ~ ~ ~ (Oe288 ~ 4e00)t(0e297 ~ 13el0)t(Oe306>> 27.30)t(Oe315>> 30.d0) ~ .. ~ pO~pg1.~ f'QO L7R)Oral) LIE TIN<j (0.324> 26 90)>>(0.333 '8.50)>(0.342>> 10.00)>>(0.351> 4.70)>. (0.360>> 0 10)>>(0,369 '4.90)>>(0.378> 7.90) (0,387 -11 00) . ~ F ~ ~ ~ ~ ~ aF Ru N RP 70 5 e 4 I ~ o F %<i' 97 9
- 0) >(0.414>>-13.10) >(Oe4Z3>> 12.40) ~ ~ ~ ~
'0.396>>-IR.10)>>(0.405>- (0.432>-11.80)>>(0.441>-11.9 0.450>>-ll.d0) >(0.459> 11.40) ~ ~ ~ ~ (0.468>-10.90) ~ (0.477 ~ -9.70) ~ ( . 6>> -8.10)>(0.495> -6.60)>> ~ (Zog (0.504>> 5.00)>>(0.513>> -3.30) >(0.52 -1.10) >(0.531>> 0 ~ 0 )>> . ~ (0.540 ~ 1.30) ~ (0.549 ~ R.OO) ~ (0.558> 0) >(0.567>> R 00)>> ~ ~ (0.576>> 2.30) ~ (Oe585>> Ze50) ~ (0.594 ~ 3el (O.d03> R 50)>> ~ .. t 0.61R ~ 2.60) ~ (0.621 ~ 2.10) ~ (0ed30> 1.90) ~ 39 ~ 1.10)>> (0.648>> 1.30)>>(0.657 ~ 0.90)>>(0.d66> 1.00)>(0. 0 0 )>>... (0 d84>> -0.20) (0.6S3 ~ -1.00) ~ (0.702 ~ 0.80) (0.711 .10) ~ ~ ~ ~ (0.720 -0.70) (0.729 -0.90) (0.738 -1.20) ~ (0.747 -0.7a (0 75d>> Oe0 ) ~ (0 765> 1.80) ~ tO 774>> R.90)>>(0 783 ~ 3.20) ~ (0.792> 4.10) >(0.801>> 4.d0)>>(0.810>> 4edO) t(0.819>> 2.90) ~... (0.828 ~ 2.40) ~ (0.837>> 2 10)>>(0.846>> 1.20) >(0.855>> 0.70) ~ ~ ~ . (0.864>> 1 10) t(0.873 ~ 1.00) ~ t Oe882 ~ 0.80) ~ (0.891>> 0.0 )>> ~ . ~ t 0.900>> -0.30) >(0.909 ~ 0.10) ~ (Oe'918>> 0.30)>>(0e927>> 0.80)> .. ~ (O.S36 1.10),(0.945, 0.80) ~ (0.954 0.40),(0.963 1.00)>> ~ ~ ~ t O.S72 ~ 1. 10 ) ~ ( 0.981>> 1 ~ 10 ) ~ ( O.S90 ~ 1.70 ) ~ (O.S99 ~ 1,80) ~ ~ ~ (1.008>> Ze00) ~ (1.017>> 1.90) >(1 ~ 026> 1.50) ~ (1 035> 0 90) ~ ~ ~ (1 044>> 0 ~ 0 ) ~ (le053>> -0 ~ 70)>>(1.06R>> -1 40)t(1.071 ~ -2.00)>>" ~ (1.080 ~ -2.50) ~ (1.089> -3.00)>>(1 ~ 098>> -3.10)>(1 ~ 107 ~ 2 90)>> ~ ~ ~ (1 lid>> 2e90)>>(l 125t 2 ~ 00)t(1 134>> 0 ~ 70)>>(l 143>> 2.90)> ~ (1.152 ~ 4.10)>>(1.161>> 3.30) ~ (1.170>> 2.40) ~ (1.179>> 1 50) ~ ~ ~ ~ (1.188 ~ 0 90) ~ fl.197, 0.70)>>(1 ~ 206 ~ 0.50) (1.215, 1.60) ~ ~ (1.224>> R.80) ~ (l. 233>> 2.00)>> (1.242>> 1.10)>>(1.251>> 2.50)>> ~ (leRd0 ~ Ze00) ~ (le269t 2 ~ 00)t(leR78 ~ Zel0)>>(le287>> 2.30)>>" (leR96 ~ 2.80)>>(1.305>> 2.90)>>(1.314>> 2.20)>>(1.323 ~ 1.80) ~ ~ ~ fle332 ~ 1 10) ~ (1 341>> 1 20)>(l 350> 0 70)>>(l 359>> 1 00)>> ~ ~ (1 368t 0.10) ~ (1.377 ~ 0 ~ 70)>>(1.386 ~ 0 ~ 70)>>(1.395>> 1.00) ~ ~ ~ (1.404>> 0.0 ) >(1.413 ~ -0.40) ~ (1.422> -1 ~ 00) >(1.431> -0.90)>> tle440 ~ Oe90) ~ (1.449>> le40) ~ (le458 ~ le00)>(le467>> 0.0 )> ~ ~ ~ (le476>> 1 00) ~ (1 485> 0 ~ 0 )>(1 494 ~ 0 30) ~ (1 503> 0.60)> ~ (1,.512 ~ -0 70) ~ (1 521> -0 30)>>(1.530> -0.40)>>(1.539 ~ -0.90) ~ " pJ ( je548>> -1 20) ~ (1.557 ~ -1 90)>>t1.566 ~ -2.10)>>(1.575>> R.50) ~ ~ ~ ~ (1 584>> 4 ~ 00)>>(l 593>> R 80) ~ (1 602>> -2 dO)>>tl 611>> 3.70)>> ~ ~ O (1 d20 ~ 6 50) ~ (1 629 ~ 8 00)>>(l d38>> 8 90)>>(l 647> 6 00)>> ~ ~ QO (l.d56 ~ -5.50) >(l.d65> -4.90) ~ (1.674 ~ -3 90) t(l.d83 ~ -3.40)>ee (l.dSZ>-3.)>>(1.7>0.)>>(3. >0. ) ( PARAHETER H=11264e >H= 76e00>DAHP=Z>>ALP=e752 CONSTANT RHOL>>-1.94>>A=1. >>L=ll. >>CD" -7 0 7> INITIAL I C=O.OR>>t K>>H) >>>>>0.5>>OlQO>> INCON RZ=5 >ROZ=O ~ >XOZ=O ~ tXZ=O ~ ~$ lf ' DYNlOIIC P=AFGEN(PKHU>> TIHE) PBHPIN=>>)5.33wP RDD=(POHPIN/RKOL-1.5wRO<<w2)/R 'I RD=INTGRL(ROZ>>ROD) R=INTGRL(RZ>>RD) PROCEDURE AVACC>>AWEL -" AA(R>>RD>>RDD>>L>>A) AWEL=2.wRww2wROw((l.+(L/(RtA))ww2)ww(-.5)-(l.+(S~wL/(RtA))ww2)ww. ~ ~ (-.5) )/(RtA)ww2 AVACC=(Rww2wRDDt2.wRwROww2)/(2.w(RtA)ww2) IF (TIME .GTo 1.7) AWEL-"0. IF. (TIHE GT. 1.7) AVACC e 0. ENDPROCEOURE XOD~(l.lw3+10w2.3wAwAwLwRHOLwAVACC+ COwAwLwRKOLw(l.lwAWEL- XD)w" AM(l.lwAVVEL-ALPwXD) HwX-CwXD )/H XO=INTGRL(XDZ>>XDD) X=INTGRL(XZ>>XD ) VHXD=AVVEL XO PRINT X>>XD>>XOD>>R>>RO>>RDO>>P >>AWEL>>AVACC TIHER FINTIHs2.700>>PROEL=.009>>OUTOEL"-.009 RANGE X>>XO>>XOO>>R>>RD>>RDO>>P>>AWEL>>AVACC>>VHXD TER HINAL END STOP /w I M% ~ <Ha '%4 rp, STONE G WEBSTER ENGINEERING CORPORATION CALCULATION TITLE PAGE %SEE INSTRUCTIONS ON REVERSE SIDE a 5010 64 IF AONTl N IAQAgP QC) HA WJC - hJMP2 PAGE I OF CA LCULATION TITLE (Indicative of the Objective): QA CATEGORY (g Dgg(g( gNI P g AhJA I.Y&l5 P~P $ 25 Vj&GP I NUCLEAR SAFETY RELATED 4VPfZOPyd+NIIC LOAG5. Q~ Qm 0 OTHER CALCULATION IDENTIFICATION NUMBER CURRENT OPTIONAL OPTIONAL J. 0. OR W.O NO. DIVISION S GROUP CALC. NO TASK CODE WORK PACKAGE NO. 1~I-r7 Ze efvIP/ EC5 0(-2t 55 $2 A + APPROVALS SIGNATURE 6 DATE REV. NO. SUPERSEDES CONF I R M AT ION OR NEW + CALC. NO. + REQUIRED (4) PREPARER(S)/DATE(S) REVIEWER(S)/DATE (S R VIEWER(S)/DATE(S CALC NO. OR REV. NO. YES NO SQJ1l we( 5 z/d'g ~/~/~7 CJc.. + . Ns-l8~v ~ 2, DISTR I BUT ION ~ COPY COPY GROUP NAME 6 LOCATION I SENT GROUP I NAME 6 LOCATION I SENT RECORDS MGT. FILES (OR FIRE l7OC ~IITac L WAFLE IF NONE) ~ 4I II ~ 7j $ 'P,' ~fl PIY ~ .t 8 s'~ '4 *< 'L7 'rj (R STONE e WEBSTER ENGINEERING CORPORATION CALCULATION SHEET 4 5010.55 CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. l>1~7 We DIVISION & GROUP PQP y.g- >155'l CALCULATION NO. OPTIONAL TASK CODE P PAGE 3 TABLE OF CONTENTS l2 I, T1TLE PA 6 K l3 14
- 2. TP BEE DF c.oNTsvT6 2 RRYISlOA QATIj( -3 4, lAYR,ODUCTIOH / SAC,<4goOgp
- 5. OP. 3E.CT I VE N suHPai oaa 24
- 7. CDMPUTBR. PR06gpbh ID
- e. HB'TAO'.
02&IC hJ 1NP UT 29 30 lo. cbocLUy lol5
- 11. CONNAP y OF P.& OLT5 l2, RFFEP.BMCBS 8 ~ ~hi ~LY&l5 2.(
- 14. CO+pgye g, LOG gC cs tv/ Inm P IC uC ATT~wmys I. Cg MP F'MARP lh US TI WC
~ 7 ~ t IF% %,4 1 I I-I ~ 1A 1+)I% V' IL<fg 4>ltllld, t f..VISION STATUS TABLE PAGE ND. CAI CULATIONNO. I~'>>2 ->><'> >< 7750 JOB ORDER hi/. lg REASON NON-INDEPENDENT INDEPENDENT REVISION/DATE / REVIEWER DATE, REVIFWFR /DATE APPROVAL/ DATF I~.> .a'a yl al 4 rr r r
- a. ~ r
;.t> ~ I'i>t ai 'l}ai r; ~ i(I, '. .'i r... ig'- j; I ~ I~ ~ ~ ~ I 'i . I la a,h.,g '1 r'g, ~ ii:'.r . r) III I ~ )(r,,) gA )4 f l 1st 'L p gt e STONE B WEBSTER ENGINEERING CORPORATION CALCULATION SHEET X 5010.65 CALCULATION IDENTIFICATIONNUMBER DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE 4 J.O. OR W.O. NO. (g.l 77, Q.Q /MAL Ilhl' >l55
- g. IgTgzyuCTIOe/ SPCrCXOuVCI:
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- a. 46 Cl IE USMC PROCjRP ~ Tt) g~T p p 22 <<SP~<SF- OF f POP 5~5~g M.
24 I5 tact-OPSY I 8 TW ATT>cH-HetdT- J . 26 27 28 5I 40 4I 45 45 lL A a+4 $t ,4 1 STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET L 50I0.55 CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE V<- ~I S.S. M/S ETHOD o TH I5 GA I.GUl ITIOUS 0&65 'TW CISIVlE, VPTHGNtPTICA I HOCBL OF C~ QQWQCOHCR. WQp 4p ME WQAL /7'IcPI. IO B E'THOU A5 V609 )N TH5 gRICIIIAl C&LCUI AT(OA CIIcF I) THB OhJ I 7 CHP HE'S P RF 1 HE 5 gV ~hid CO t'H pu 13 >HPuv Lope)as. voc.uH<dtep >v K&F. g. Tee l6 S~H6 .T IMG W-l&TaRV I N AI.QSI5 i5 PO~B P~R 7H-8 IS py~~ 0~6K UG>H4 5zp,g.gyHB Cggpgtl-f- coP8 . AS l9 REF. i > lg P,Pg iTIud TO 'fHPT 4 SINFUL E t eaSC~ OF FaeCVO' f 4V~F) MOC SL tg e~7~8t,I~Mao TD ~DV4T 50& T~ FI.UlV 5lROCYUPG Ir47ER.PC,Trod tuR<N4 SRV(REI:.6) & CO LC)~C CVE.HT. A PETPILfp PSST.IPTIOH QP THE Qh)P,j fylC,P t ~op< 30 OBJET)HEP lk RBF. $ . 3I 3S 37 I'g h, I) '.5 i'tfi pJ [I STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET 45010.55 J.0. 0 R W.0. N 0 l~i~a. ~% CALCULATION IDENTIFICATIONNUMBER DIVISION 6 GROUP CALCULATION NO. g(-wi55 OPTIONAL TASK CODE Q]A PAGE ~
- 9. DESIGN Id~uT; Q. I DC) WrJ C atoll Cz, DATA~
P P &BP Gw R&t-, i TH6 PDuvdcoMGR P~PGR,TIFF AR.G 10 FOLLOW5: 12 MATBQ1AL = Qp SI2 TP ~04 13 14 ~IZS = 24" GCH 2,0 F'IP8 15 16 iP ~ R3 25" 16 Gy 2.4 19 Ce'<R~< ao Of'RDSS 484TIOt4 = R7 g3 i 22 Sg/'VI g M n!gggLgg . = Igl ' 24 LE'A6 THCI OP TH% POWhl COSMIC R.S VP,gf ACGORIOJNQ TO P(6. i,. 31 36 40 44 4$ 46 t>' !p gl tl )9 I yif A S4 'I [i -1, fl' pl STONE & WEBSTER ENGINEERING CORPORATION CALCULATION SHEET 4 III0.IS CALCULATION IDENTIFICATIONNUMBER 4.0. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE~ CHP hh(- ~le PA OHthfC HER G&~a' FCEV g. 4" c M Apr QIALL %yegg! gs FATS rv/ IO I. 27. 4D $ 5a W'. l2 Z. l7. 4~ P~r~c) $ 45'o oo /N. X7.83 rt seri~/sr+muirw) S/ce jr. /H'C. l4 ~iom/Fr. (arwrsc) /8B 8o tit4r. IS aoerkT m /~iw /8+2.0 W+ 4rc7icwV HctlvLirg /~/ 9 re~ g$ Cd a t]A /N'6 Rh~ / 20 2:D o.a. '4A5'-aO iS/. zH. JeNCL Pf/4C aOfS D 5W. 24 4 C~ETifc) $ 8.+8 ear, 2$ Ws/4W jar /SS.W ~~ 24 Dal/SIMP' 0, Z95 ++a FHV. IR - 0 )0 DELTAIC FLFg /%-0 El.av. A ~ AS 44'- CI A l: au'-o 45'-CI 8-I e'-o as-) 40 a ~.~- - 44 Hove 2 AS DKI4eteS CelWHC~'+~ AC. Scabs ~@co~~ ~~ 4<'~~+~~~~ -~ ~' 4I ~
- j. ~M,~ ~'g~r
h l,g ~r ' yd t t yl k STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET 450IO NI CALCULATION IDENTIFICATION NUMBER 4.0. OR W.O. NO. DIVISION & GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE I 2I 7'7' FMP 5 5LS HS,- 2I P g - FSC'I! LavfS/EV&r COAr8n/87/DAIS AHD AeaPPtAeE 'AreRM 7~ LNp/EP'Wr CW/PTIOhlS /A/D ]0 CCEP7ighCf M!7ERJA FPE 77fs DoenJcontFZ AMrp'sos pA'F Zwssp on/'idcz4p 2-I IO OcPI'AtP-2 FSAE ()PFF. 7) .III SECTION M~ Tkf DESsGAI ZOaD/n/CS Oa SWV r n/4 C'0 HZ'on/SeVWrieCV Z~eC~D IS l4 7o JHtPC]FY 7'M/YS/S . 15 T'/lE 74furr.rued(zs) F wr cn~pu~r>ac t~ reals'.2 i (EzR T) )OAT RFDIJCED TO 7ffE /=OCCOW46 FOrJR(4) 6ONel//J$ , ~il7/ccHD ~8MTiaN$ F'os lJPSF'7 Con/air/onj 7'oe/@calf~ An/AcYs/s: t4 A'SZ ~SRV SPRAT &EA?GEAlc'Y C'on/ i / h! N'~ O9E'i SRV ~ S&'/Saw~~ tt SO F4VL c b Sl FAdL7Q Z.- A!t SSE' $ 'IV +CO l~) S4 FAucrED J. - 5'+ SsE>> IBAJDNe~o &) SS SO 40 14 1I Il I% I I "I'd ~a gl g4 l~ STONE B WEBSTER ENGINEERING CORPORATION CALCULATION SHEET A 50I0. CALCULATION IOENTIFICATION NUMBER ej }%17 'l J.O. OR W.O. NO. DlVISION Fs GROUP CHl EQIS CALCULATION NO. OPTIONAL TASK COOK PAGE IO 9, 2 - DEsr cu sac caririsiw~ rrorIrs waP Accnraecz crruww <oe 'P) 7iVQF lRMi? 6OVFNlhl4 LAD QA484kf7iOrIIS NE'POHPE'D) IHccvnrNG Ter- co&ponlz~z oF'scrsmrc, slav. HArD LocA loAsr4GS TNT NE vsse Fare'N ader pcs~ As Foico>$ - IO lJRFET or 7)on/ 12 y+ (awe i ouz) + (zwvs IS ~zevz)'EZGENc l4 Cokbi i rod'/~ l6 (olsuz OBESE ~($RusiÃY4l cuur,e +Nd$ ss+ cAufs) ucw) ouDr Tro4 l9 , h'i (SSZZ-SSrSI'~(SeZ<<~SRq)i(COs-COSS) -SFE uurui (A) 2S 26 (sssz ssus) (suus see)'i( wuu,', cyuge' ouucs) (4A) 27 s'hBPP: 20 2$ Co~ Co z~~r~ ~D 50 CO ss 5 UBMFR~ 5 TA'VC err,'F La4$ Af uoA'awe or~rieG cours(muser, ysermnr~i) 12 08ES ~ 0'HSR7/A = Cr+E SL,PSP/A'G LoA8 LCM'gFg SZFZ ~ SSE ZnlBPT(W LoAD $5'ES = SSF S'LOSHIN6 LOAD 16 ZFVS = Sti/ su8@seED srecWRz avaScFcoln DR VL DWV In/ERMA LOAD Ch'uF ~~ CHV86rNG L47ZR'AL LOAO Ch'UG gg = C HUGC)Ale SUSAEZCED STAPUCTclRE lCvtO 40 CHUG z = ClvGG/HG Zn/ZIZZ 18 LOAD Ar'esZ r SR'tS' rS rVr$ 5m~<~ seWiiiv @WE-~~ ~=~c,F SPY z~iVoN~ nr ~zs7 W~4~ AS cu~.'M&7nb+i-Wct nrY~W "ZW v rs m~ Fe'v~~a' Sk Vdwig Sf Vow, SR4i'j, aaa 4$ ~~J zcc 46 g~l ~ I, t~ Wl p I 4V STONE & WEBSTER ENGINEERING CORPORATION CALCULATION SHEKT 4 5N0.4$ CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE il Gee HV ws-~ITS DFSI CA/ LOAD OMEGA/8 7 O4$ AND kC'CEPXÃAICE'R!TfX,'IA COE2 'd 7'oAPxud'o&BAA7ionlS ]N SCP. (2A) .7eCoUDW (4A.) 4ZF b5FD Foe 7vE bOWA/C+VaAR. Aacrzrs IO 7o ezrr yWE RF47drR&t&JTS N'hE Fouoewg: l2 (/) - C'sos 2 Pzpzea AMcysls w' cccranwacs @iTN szcrroN )AC- 96'Ce Oi PE zr. (zzs ]o) AS'CIK, (2)- >=uacrionl~>. cE>>>>e>c>ry E~~>.ys>s >u EccoeDE>>c=- N J TH THE h'RC R Gucwroer posizim i4 gEEEEBVCE >/ EAID A/EDD -N >F85'M>>: 2 ) 19 20 22 24 ts 29 29 29 50 51 99 4 I~ f 'I a STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET X 5010.55 CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. DIVISION & GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE I W 71 Ego/Pk< MC - WISS Al A g.3 OYNAMIC LbAPIHN I~PUT 's PGgB'hJcB& F.Dg iNPUT 'sly P4)P Co LOAD5 P P-E 10 P,S, Fo ILow5: 12 SRV- SL)8tvlCRCiBD STQIICQIIRE. LDII'D)NI2 %SF 13 (2) +0 &0 5 HQII~SD 0<RVCTlI125 LDADII452 IIBF:: 4, 7. 15 16 18 19 23 24 2T 28 29 30 31 32 34 38 402 41 22 *l~ iC 1 4.P /'g f.'y .J f STONE 8 WESSTER ENGINEERING CORPORATION CALCULATION SHEET 4 5010.55 CALCULAT.ION IDENTIFICATIONNUM8ER PAGE ls J.O. OR W.O. NO. DIVISION FJ GROUP CALCULATION NO. OPTIONAL TASK CODE I>1~a ~V S~P ah(- >I SY N
- 10. CQtd CLU&1045:
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SUMMARY
Tp gag (g) UNITS IN KSI UPSET CONDITION EMERGENCY CONDITION FAULTED CONDITION MODEL (Al) MODEL (AO) MODEL (AO) LOAD CASES Qn~l.55 HZ Vn~1.94 HZ Va~l.94 HZ SEISMIC INERTIA AND SLOSHING (a) OBE 8 16 7.27 (b) SSE 14.46 (a) SRV SS LOAD 13.13 17.43 8.2 FAULTED 1 16.48 FAULTED 2 (b) SRV ARS 0.30 0.30 0.20 (a) CO SS LOAD N/A N/A 18.15 (b) CO ARS N/A N/A 0.68 (a) CHUG LAT. LOAD N/A 9.68 8.49 (b) CHUG SS N/A 9.20 8.79 LOAD (c) CHUG ARS N/A 1.16 0.90 N/A N/A 0.30 TOTAL COMBINED 15.72 24.04 25.18 FAULTED 1 STRESS 25.68 FAULTED 2 FUNCTIONAL CAP- 31.26 FAULTED 1 ABILITY ALLOWABLE 34.35 %.Q. -UDICED 2
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CLIENT 6 PROJECT PAGE I OF TP NxwygR WOHRulK POCum M/n/Zu4 AZC~ POZ~~t- DNA Z CALCULATION TITLE (Indicative of the Objective): QA CATEGORY (1/) I NUCLEAR dowsrus+7/Oy ~tu ~r/O~ iowa= Pg SAFETY RELATED AIC?Oh'EBS PA58g OP /1/~ P Z Pl~//7 SR~I ee I C Olz Q~ 0 OTHER CALCULATION IDENTIFICATION NUMBER CURRENT OPTIONAL OPTIONAL J. O. OR W.O. NO. D I VISION 8 G RO U P TASK CODE WORK PACKAGE NO. GAL C. NO. 44 lZ j 77.za APPROVALS - SIGNATURE 6 Pl I'Cc DATE
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STONE L WEBS>ER ENGINEERING COR>ORATION CALCULATION SHEET CALCIA ATION IDENTIFJCATION hkA43ER JO. OR WO. NO. DIVISION 4 GRIP CALCLKATION HO. OPTIONAL TASK CODE PAGE 2 12177. ZS NP {C) pP- du/bd-o STATnmn OP REVIEW This calculation has been reviewed in accordance with CBOC ENDS 82-l2 and was found to be adogQate ~ The aIethod of review was: (list the appropriate itens)
- a. Review of Calculation
- b. Comparison with a sisLLlar previous calculation
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REV ZEWER NETBOD 2~ REVIEWER 3~ REVIEWER defied The statement below applies to Nuclear Safety Related Qh Category I calculations only. This calculation has been INDEPENDENTLY reviewed in accordance with CBOC EKN 82-12 and was found to be adequate.
- a. Ccxaparison with prequal aethod and assumptions (pr equalif ied document nuaber (s) )
- h. lddressing the key questions appoariny in KLP-5.3, and EJLP-3.1 (latest revisions)
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/9/77.gg /Y/ CGQ f g-40/do-8 TABLE OF CONTENTS Section Title ~Pa e TITLE PAGE STATEMENT OF REVIEW TABLE OF CONTENTS IO REVISION STATUS TABLE 12 1.0 OB JECTIVE 13 2 0 2hl 7Rd DU~IdN ('o 14 3.0 ASSUMPTIONS ..F IS P.P METHOD 9 l6 5.0 DESIGN INPUT 18
6.0 REFERENCES
7.0 RESULT
SUMMARY
23 24 e.p COMPUTER LOG 9.0 MICROFICHE 74 26 ATTACHMENTS 26 29 C PyJ $ V('T'f 7C5 7 RESVL,'T5 I 31 5 PER(F(~TI~IQ oP C.S~Io PRa~~ 6(- gq 32 C. Lo ADS oW bo~ 4 1"-0&CD. ' W pgp~7AL 33 C ( C l7 35 Poow (FRog P.Ep, I'I') D f HPu T L(sg(rd g D(- DS-39 E. PR5 CA3AAg(g'd 4 F 4 TC o RAM DNA '4 43 4T/C4/12210/55 46
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STONE 8 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET L SSIO Se CALCULATION IDENTIFICATIONNUMBER ZS'I J,O. OR W.O. NO. IZI77. DIVISION 6 GROUP uJ CALCULATION NO. PX- bdldO-O OPTIONAL TASK CODE PAGE I.0 OB JECTIVE The purpose of this calculation is to provide submerged structure loads on: Q SRV discharge line and quencher Dovncomers Io Q SRV vent lines Q Piping supports I2 I3 Q Miscellaneous (discharge and suction lines vith strainer) piping 14 due to: I6 Q LOCA bubble Q SRV bubble I9 Condensation oscillation Q Chugging Q Seismic sloshing 24 Q Pool avail and fall back Q LOCA jet 2T 2S These loads are to be applied to the structures for response assessment. 29 30 co/ cm/o,d<ag N+l/'2 p<nn9 spec( f'c. Co Lo-"o(a a/el<in 3I 32
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- 2. INTRODUCTION Loss of coalarit accident (LOCA) is a design basis event for boiling water reactor (BWR) nuclear power plants. Following a large break accident, the drywell pressure will increase rapidly due to the steam or hot water released from the high energy line break. For a Nark II plarit, such as NNPB, the pressurized 10 air-steam mixture will be pu7 ged through the vertical downcomer irito the suppression pool, where the steam content will be l2 condensed. First, the suppression pool will swell and the drywell air purged into the wetwell. High steam mass flux with some residual air blow down will occur following the pool swell l3 l4 arid fall back. Initially, the steam massfaceflux will be high l5 enough to prevent the steam-water inter from r center ing into I6 the dowricomer. The dynamic pressure oscillation resulted from the I7 oscillating steam-water interface may generate dynamic loading on the contairirnent as well as on st7.uctures submer ged in the suppression pool, the load is called the condensation oscillation l8 1 c ad. As the blow dowri cont inues, the steam mass flux as wel 1 the air content are further reduced, eventually the steam caridensatian becomes unstable arid water'eentry into the dowricamer will take place. This phase of the blowdown is 23 characterized by cyclic steam bubble formation and collapse at the downcomer tip, the phenomenon is called chugging. Chugging 24 also gerie7 ates dynam'oads on containment and submer ged structures. Test series 5288 was conducted at the temporary tall 26 tank test coridensat ion oscillation (4TCO) test facility at 27 General Electric Company to investigate the CO phenomena. The Nark II gerier ic CO and Chugging load definitions were derived from the CO and Chugging test data obtained from this test series 28 29 30 respect ively.
3I 4TCO test matrix was coristructed in such a way as to envelop 32 all the possible LOCA conditions, which covers different reactar Inadels, nuclear steam supply and coolant systems, and different suppression pool temperature operating ranges for all Nark II 33 34 plaritsl it was also constructed with the smallest pool area per downcomer for all Nark II plants so as to obtain conservative 36 dynamic pressure measurement. These conservatisms were noted and 37 acknowledged by the NRC (Ref. 7 8, 19). In particular, it was faurid that the transition from CO to chugging can be defined in The generic. Nark II CO load 38 terms of pool temperature. definition did not take credit for bath;theacil,=-'s(ze and- the NRC 40 pool temperature effect in defining the"CO"-'X6ad; .'h'awever~.the - 44 allows individual plants to take credit ef.'these.-effecti--(Ref. 19) 43 46
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STONE B WEBSTER ENGINEERING CORPORATION CALCULATION SHEET L 5010.65 CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO.
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CALCULATION NO. p~- ~D/60- 8 OPTIONAL TASK CODE PAGE ~ 2', livTR'oudcT/oH C CoNTD) A poo 1 t ernper at ure t r ans i ent f ca 1 cu1 at i on has been per orrned (Ref. 2I I), temperature it at was found that the maximum anticipated bulk pool the trarIsition from CO to chugging for NNP2 l2 following a DBA event is 119 degrees Fahrenheit. Allowing for I3 additional margin, a 138 degree temper ature limit was established 14 to def ine bounding por t ions of the 4TCO test data used for the IS NNP2 CO load definition. GerIeral Electric Company defined. the CO I6 load for NNP2 based on a pool temperature limit of 138 degrees Fahrenheit (Ref 12). This means that 4TCO test data that are outside the operating temperature limit are excluded from the I6 data base. This approach involves the compilation of 4TCO data l9 below 138 degr ees, gerIerat ing a power spectr al density (PSD) erIvelop of this data, and developing a number of new 4TCO time ( 22 history segments to match the r>ew PSD envelop. The bounding 4TCO time history segments are used in this calculation to calculate the submerged str ucture load on downcomers. This calculation uses the same -model and analytical method as the original calculation (Ref 18), which calculated the submer ged structur e load for downcomers in NNP2 pool using the generic Nark 26 II CO load definition time segments. The only change made in 2T this calculation was the bounding time history segments. 26 The bounding 'time segmer<ts for NNP2 CQ time segments were 29 presented irI Table p along with the generic Nark II CO load 30 bounding time segments for reference. 3I 32 33 34 36 37 40 44 43 46
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$ .0 ASSUHPTIONS The flow in the suppression pool is incompressible, irrota-tional, and inviscid.
The pool boundaries are rigid and water surface remains stationary.
- 3. Flow field perturbations due to the presence of submerged structures within the pool are negligible.
10
- 4. The incident flow is approximately uniform in the vicinity of a 12 structure so Horrison's equation Q'.I.Ignis applicable.
13 14 15 I' 1/2 CUAU IUI + C f VS du dt 16 Where: = Density of water 17 18 CD
= Standard drag coefficient A = Projected area normal to the flow field U = Velocity 22 23 VS = Structure volume 24 C
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= Inertia (acceleration drag) coefficient 25 26 5. For CO, chugging, and LOCA bubble load calculation, method of 27 images (HOI) is used by approximating the annular pool geometry 28 with the rectangular box in three ways (Figures 1-3), and 29 cylindrical pool is approximated by a rectangular box shown in Figure 4.
30 31 34
- 6. The hydrodynamic interaction between annular and cylindrical 55 pools through the vent holes is negligible.
37 7. Drag volume for a finite cylinder in axial flow is conserva-tively approximated by a disk and the displaced volume. 39
- 8. Structures are rigid and small compireC':~W>> he. Zhata6teriitiz.
40 length of hydrodynamic disturbance~=~"-.-.fliizd=,structure 41 interaction effect is negligible....==.= -,-.-~=:~-",, -..'~ ,.=.". '-'..-'
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pv-4o/ga-0 OPTIONAL TASK CODE PAGE ~ 4.0 NETHOD Calculat iori of the submerged st7 uctu7 e load on downcorne7 during the Ca phase of a LOCA event is performed in 3 steps. First, the volumet7 ic flow field caused by the condensat ion oscillation of the steam bubble is calculated from the dyriamic lo pressu7.e tr aces, then the flow field and the iriduced drag loads ar e calculated for the ta7 get downcomer. Procedure to calculate the volumetric source is described in sectiori 4. 1, that of the l2 l3
'low field and the d7 ag load calculation are desc7 ibed in section
- 4. 2.
I4
- 4. i Calculatiori of the CO source strerigth I6 I7 The bottom center p7 essut e data at the 4TCO tank were I8 provided by GE '(Ref. 1.). These data represented the actual pressure reading dur ing a simulated LOCA blow down event, the data corisists of hydrostatic pressure increase as a result of the wetwell airspace pressure iricrease in additiori tc the dyanmic p7 essure coI-responding to the CO phenomena. Since only the dynamic pressure will induce drag loads on the subme7 ged structures, trend removal was performed in 24 reference 22 to extract the dynamic pressure for the 25 bounding t ime segments of NMP2 CO load def init ion.
26 Table 1 provides the data set names for the trend removed p7 essure data for the bounding time segments 27 arid its associated 4TCO run number and lug/t ime periods. 28 29 The volumetric sou7 ce strength, SDOT, is related to the dynamic pressure oscillation, P, in according to the 3I fol lowing equat ion (Ref. 1): 32 34 SDOT = S = P /it f(r) Cft /sec 3 wher e f' wat er density Ls ft3 f (r) = 4TCO tank constant t:ft I 3 38 t = time Csee} 39 40 The volumetric so urce produced by the s team S S, b which';.i'-WQW.:mokumj..t2 ~f~ iorr~~m';.-4h~l2a~~
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STONE 6 WEBSTER ENGINEERING CORPORATION CALCULATION SHEET 4 5" 10 6$ CALCULATION IDENTIFICATIONNUMBER I J.O. OR W.O. NO. DIVISION C GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE N P (~) pq-(.OI ~0 -o f SS = (p / f f(r)) dt Lft ~ /sec3 The quarItities SDOT and SS are computed from the dynamic pressure traces usirIg the IBM simulation language CSNP ( Ref. 23) . IO Since the 4TCO test matr ix was constructed to simulate the Nark II plants'OCA blow down conditions, it is l2 expected that the infer red CO sources from the above l3 equat ions using the 4TCO tarIk constant are applicable 14 tc Mar k I I plants, NMP2 in part icular. I5 I6 23 26 2T 2S 29 3I 32 34 33 37 40 , 44 46
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- 4. 0 METHOD (cont inued)
- 4. j?, Flow field and drag load calculation Flow field in the suppression pool is calculated by the computer program SSLOAD (Ref. 11). This program solves the Poisson' equat ion with point sources using the method of images (MOI) (Ref. 28). Since MOl is applicable only to flat boundaries,'he annular pool is model led as a parral lelpipe. Thr ee rectangular boxes are constructed to approximate the suppression pool as shown in Figures 1-3. Flow fields and drag loads are calculated for each of the thr ee rectangular boxes, the box that produces the most conservative load are presented as the design load.
The number of images used in the vertical, radial, and circumferential directions are 22, 11, and 3, respectively. CO sour ces are apprc x irnated as point sour ces at one foot (. below the the downcomer tip, wher'e the steam-water inter face is expected to be located. One source is assigned to each downcomer, and all source are assumed to have the same source strength. Since the CO sources are not expected to be oscillating exactly in phase, the flow field is calculated with the worst phasing assigned to the CO sources. That is, a time delay is assigned to half the pool so that the peak negative pressure within the fundamental CO period coincide with the peak positive pressure of the other half pool. The pool is divided at the location of the target downcomer. A sensitivity study was performed to locate the downcomer that would experience the highest load. Downcomer 43 (Fig. 4) in the annular pool was found to be the worst case location. Flow field and drag load calculation wer e then calculated for this downcomer. Once the flow field is known, the submerged structure load is calculated u sing the.Norr ison's equation described on page 8 (Ref. 28) . Ad J ust ment ar e made for intaiflar~~ffeeM 'and.;unsteady
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IZ I 7 7. Z8PC<) J.O. OR W.O. NO. DIVISION D GROUP CALCULATION NO. pE- 60/Cud- 0 OPTIONAL TASK CODE PAGE Method - The pool is approximated unwrapping one-half of annular it byinto 1 pool and transforming a rectangular box with the shown dimensions. R~= V C. I 7 tEAh'ADIIV~ l2 l3 I6 17 I8 I9 R7 20 21 22 24 I / ANNvLAg POOL 2S 26 27 26 30 3I 32 34 RZ- RI 37 T'P'~S F okapi RE c Th73 GI3 L. A R:-ScI;~~~~- ~~:='" =~.-'-'."
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<<>>>> DRAG LOAD SMEARY <<>>>>
DRAG LOAD5 NORIIAL TO T)IE 5KGHEtlT AXIS (LBF) III CARTESIAN COORDINATES CYLINDRICAL COORDIHATKS 5KGIIKHT 5KGHKHT HUIIBER X Y 2 RKSULTAHT AHGLEIDKG) RADIAL TANGENTIAL VERTICAL RESULTANT VL 329.dl 732.67 0.0 803.40 162.00 -87.06 -798.67 0.0 803.40 252.87 554.27 0.0 609.23 162.00 -d9.22 -605.28 0.0 609.23 181.99 395.07 0.0 434.97 162.00 -50.99 -431.97 0.0 434.97 122.28 263.95 0.0 290.90 162.00 -34.73 -288.82 0.0 290.90 70.51 151.d5 0.0 ld7.23 162.00 -20.19 -166.01 0.0 ld7.23 23.05 49.4 t 0.0 54.57 162.00 -d.63 -54.17 0.0 54.57 TOTAL 980.30 2147.08 0.0 2360.31 -2dS.S3 -2344.92 0.0 2360.31 i s~
/ >>>>>> DRAG LOAD SIARIARY >>>>>>
AXIS ILBF)
DRAG LOADS PARALLKL TO TIIE SEGIIEHT I
CARTESIAN COORDINATKS CYLINDRICAL COORDIHATES 5EGHKHT SEGHKNT HUIIBKR X Y 2 RESULTANT ANGLEIDEG) RADIAL TAHGENTIAL VERTICAL RKSULTAHT b n
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<<<<<<C.O. LOAD ON OOHNCOHERS PX-40052-2s RUN 07ol2-14 SEC PAGK
<<<<>> DRAG LOAD S(N)(ARY <<<<<<
DRAG LOADS NORHAL TO THE SEGHENT AXIS (LSF)
CARTESIAN COORDINATES CYLI)SRICAL COORDINATES SEGHENT SKGHENT
)AA(8ER X Y Z REQLTANT ANGLK(OKG) RADIAL TANGENTIAL VERTICAL RESN.TANT 1 343.ld 914.20 0.0 974.48 142.00 -43.84 <<975.49 0.0 976.48 2 265.42 490.45 0.0 739.78 162.00 -39.26 -738.74 0.0 739.78 3 193.89 491.05 0.0 527.95 142.00 -32.45 -526.94 0.0 527.95 131.9d 327.57 0.0 353.15 162.00 -24.27 -352.31 0.0 353. 15 5 7d.72 188. 07 0.0 203. 12 142.00 -14.85 -202.57 0.0 203 ~ 12 6 25.18 dl.35 0.0 d6.32 142.00 -4.99 -64. 13 0.0 4d.32 TOTAL 1036.52 2d72.49 0.0 2866.78 -159.87 -2842.18 0 ' 2864.78
<<<<a DRAG LOAD SN9(ARY <<<<<<
DRAG LOADS PARALLEL TO THE SEGHENT AXIS (LSF)
CARTESIAN COORDINATES CYLINDRICAL COORDINATKS SEGHENT SEGHENT NU)(DER X Y Z RES(LTANT ANGLE(OEG l RADIAL TANGENTIAL VERTICAL RES(LTANT
<<f ul
<<a<<C.O. LOAD ON DNKONERS PX>>40052-t) Rlk) 07)lt-ld SEC+ PAGE
>><<<<DRAQ LOAD SNOQRY <<<<<<
DRAG LOAD5 NNHAL TO THK SKGHEHT AXIS (LSE)
CARTESIAN COORDINATES CYlIHDRICAL COORDIHATKS SEGHENT Y Z RESLLTANT AHCLK(DEQ) RADIAL TANGENTIAl VERTICAL RKSN.TANT 1 343.14 914. 20 0.0 974.48 142.00 -43.84 975.49 0.0 97d.48 2 245.42 4'90. 45 0.0 739.78 142.00 39.24 738.74 0.0 739.78 193.89 491.05 0.0 527.95 ld2.00 -32.45 -52d.94 0.0 527.95 4 131.94 327.57 0.0 353. 15 142.00 -24.27 -352.31 0.0 353.15 5 74.72 188.07 0.0 203.12 142.00 -14.85 -202.57 0.0 203.12 4 25. 18 41.35 0.0 44+32 142.00 -4.99 -di.l3 0.0 4d.32 TOTAL 1034.5t t472ed9 0.0 tbdd+78 159.87 -tbdtolb 0.0 2844.78
<<<<<<DRAG LOAD SNNARY <<>><<
DRAQ LOAD5 PARALLEL TO THK 5EGHKNT AXIS tLBF)
CARTKSIAH COORDIHATE5 CYLI)NRICAL COORDINATES SEGHENT SEGHEHT
)CASER X Y Z RESLLTAHT ANGLE(DEQ) RADIAL TAHGEHTIAL VERTICAL RESULTANT
' ) )gl
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<<aaC.O. LOAD ON DDHHCOHERS PX-6005Z-2 ~ RUN 09gl0-13 SEC ~ PAGK aaa DRAG LOAD SU)R)ARY aaa DRAG LOADS NORHAL TO THE SEGHEHT AXIS [LBF)
CARTKSIAN COORD IHATES CYLINDRICAL COORDINATES SEGHENT SKGHEHT NOSER X Y 2 RESULTANT ANGLE)OEG) RADIAL TANGENTIAL VKRTICAL RESULTANT 203,41 545.03 0.0 581.75 162.00 -25.03 -5S1.21 0.0 581.75 157.55 411.74 0.0 440.85 16Z.OO -ZZ.dO -440.27 0.0 440.85 115.09 292.90 0.0 314.70 162.00 -18.95 -314.12 0.0 314.70 78.38 1'95.41 0.0 210.55 162.00 -14.15 -210.07 0.0 210.55 45.59 112.22 0.0 lZ1.12 162.00 -8.db -120.81 0.0 121.12 14.97 3d.61 0.0 39.55 162.00 -2.92 -39.45 0.0 39.55 TOTAL dl4.98 1593.91 0.0 170S.52 -92.33 -1705.94 0.0 1700.5Z
<<a>> DRAG LOAD SU)R)ARY a>>a DRAG LOADS PARALLEL TO THE SEGHEHT AXIS (LBF)
CARTKSIAH COORDIHATKS CYLIHO'RICAL COORDINATES SKG))KNT SEGHKNT NU)R)ER X Y 2 RESULTANT ANGLE)OEG) RADIAL TANGENTIAL VERTICAL RESULTANT
I'P Pf i,T 0J tt lay
<>C.O.
~ ~ LOAD OH DOHNCOHERS PX-d0052-2 ~ Rl5 10s26-30 SEC. PAGE
<<>>>> DRAG LOAD SQ%tARY <<>><<
DRAG LOADS NORHAL TO THE SEGHENT AXIS tLBF)
CARTESIAH COORDINATES CYLItE)RICAL COORDINATES SKGHKHT 8EG)IEHT NtltBKR X Y Z REStl. TANT ANGLE(OEG) RADIAL TAHGEHTIAL VERTICAL RESULTANT 1 547.31 1257.17 0.0 1371.14 162.00 -132.03 -1364.77 0.0 1371.14 420.74 951.91 0.0 1040.74 162.00 105.99 -1035.33 0.0 1040.74 303.49 d78.9Z 0.0 743.75 162e00 79.03 -739.54 0.0 743.75 4 204.dl 453.84 0.0 497.83 162o00 -54.35 -494.86 0.0 497.83 5 118.21 Z60 ~ 90 0.0 286.42 16Z.OO -31.80 -284.d5 0.0 Zbd.4Z 4 3b.db 85.16 0.0 93.53 162.00 -10.47 9Z.94 0.0 93.53 TOTAL 1633.24 3db7.90 0.0 4033.43 -413.66 -4012.10 0~0 4033.42
<<<<>> DRAG LOAD StlttARY <<<<>>
DRAG LOADS PARALLKL TO THE SEG)IEHT AXIS tLBF)
CARTESIAH COORDINATES CYLINDRICAL CtXNDINATES SKGHKHT SEGHENT NUtSER X Y Z RESII.TANT ANGLKtDEG) RADIAL TANGENTIAL VERTICAL RESm.TAttT 1
4+t QC
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<<<<>>C.O. LOAD ON DD)NCNIERS PX d005e e RIN le 17-el SKC. PAGE
<<<<>> DRAG LOAD StNHARY <<a>>
DRAG LOADS NORHAL TO THE SKQIKNT AXIS IL8F)
CARTESIAN COORDINATES CALI)mRICAL COORDINATES SKOIKNT 5KGHENT
)%ABER X Y e RKsIA.TANT ANGLEIDKG) RADIAL TANGENTIAI. VERTICAL RKStLTANT 1 39e.ee 10Z4.7d 0.0 1097.Z5 Ide.00 -5d.3d -1095.80 0.0 1097.Z5 e 303.41 774oe9 0.0 831.6e 16Z.OO -49.ZS -830.16 0.0 831.6Z 3 eel,lb 550.95 0.0 593. d'9 16Z.OO -40 10 F 5'9Zc33 0.0 593.69 4 150.35 367.dd 0.0 397.Zl 16Z.OO -Z9.37 -396cle 0.0 397.Z1 5 87.35 e1 1. 14 0.0 ZZ8.50 16Z.OO -17.83 -ZZ7.80 0.0 ZZS.50 d eb.dd 68.89 0.0 74.dl 16Z.OO -5.97 -74.37 0.0 74.dl TOTAL llb3.17 e997.d9 0.0 3ZZZ.88 -198.91 -3Z16.59 0.0 3ZZZ.SS
<<>>>> DRAG LOAD CHART>><<>>
DRAG LOADS PARALLEL TO THK SEGHENT AXIS ILDF)
CARTESIAN COORDINATES CYLINDRICAL CIXNDINATES 8KGHKNT SKGHEHT MPSKR X Y Z RKSULTANT ANGLEIDEG) RADIAL TANGENTIAL VERTICAL RKSII.TANT
~ \ ~
<<<<>>C.O. LOAD ON OOWCNtERS PX-40052-ti RQi 14s25-3$ SEC. PAGK
>>>><< DRAG LOAD SENARY <<>>>>
DRAG LOADS NORNAL TO THK SEGNKNT AXI5 tLDF)
CARTKSIAN COORDINATES CYLINDRICAL COORDINATES SENTIENT SKGNENT NURSER X Y Z RESlLTAHT ANGLE(OEGI RADIAL TAHGENTIAL VERTICAL RE5tLTANT 1 337.41 059.60 0.0 '951.51 162.00 -46.1S -950.'3S 0.0 951.51 t 261.24 d72.32 0.0 7Z1.30 16'2.00 -40.71 -7Z0.15 0.0 721.30 190.40 470.46 0.0 5I5.03 162.00 -33.41 -513.94 0.0 515.03 1Z9.65 319.32 0.0 3<4.44 162.00 -Z4.dt -343.76 0.0 344.64 5 75.36 103.41 0.0 190.29 1d2.00 14.99 197.72 0.0 19S.29 4 24.73 59.05 0.0 44.76 162.00 -5.02 -64 56
~ 0.0 d4.7d 101'9.20 2402.94 0.0 2795.52 -ld4.95 -2790-52 0.0 t795.52
>>>><< DRAG LOAD SNORT >>>>>>
DRAG LOADS PARALLEL TO THE SEGNKNT AXIS ILDF l CARTE5IAN COOROIHATES CYLINDRICAL COORDINATKS SKGNKNT 5 KGNLNT NINER X Y Z RKSN.TANT ANGLE(DEG) RADIAL TAHGENTIAL VKRTICAL RESlLTAHT
J PI sr t'
<<>>>>C.O. LOAD ON OOWCNIERS PX-60052-2 ~ RNI RZsll-13 SEC. PAGE
>>>>>> DRAG LOAD SIRZIARY <<<<>>
DRAG LOADS HORHAL TO THE SEGHENT AXIS (L8F)
CARTESIAN COORDINATES. CYLINDRICAL COORDINATES SEGHENT SEGHENT NIASER X Y Z RESILTANT ANGLE(DKO) RADIAL TANGENTIAL VERTICAL RKSILTANT 292.56 792.46 0.0 844.74 162.00 -33.35 -844.08 0.0 844.74 226.38 598.08 0.0 d39.49 142.00 -30.48 -438.76 0.0 d39.49 ld5.31 425.05 0.0 45d.07 162.00 -25.87 -455.33 0.0 456.07 112.56 283.37 0.0 304.90 162.00 -19.49 -304.28 0.0 304.90 65.46 142.62 0.0 175.30 16R ~ 00 12.00 -174.89 0.0 175. 30 El+48 53.03 0.0 57.21 162.00 -4.04 -57.07 0.0 57.21 TOTAL 883. 74 2314.60 0.0 2477.71 -125. ZR -2474.41 0.0 2477.71
>>>>>> DRAG LOAD SNNARY <<>>>>
DRAG LOADS PARALLEL TO THE SEGIIENT AXIS (LSF)
CARTKSIAN COORDINATES CYLINDRICAL COORDIHATES SEGIIENT SEGHENT NUII8ER X Y 2 RESLLTANT ANGLE(DEG) RADIAL TAHGENTIAL VERTICAL REQLTAHT TOTAL
't t
WTP A
<<<<<<C.O. LOAD ON DQKO)IERS PX-40052<<2>> RNt 24>> 6-10 SEC PAGE
<<a<<DRAG LOAD StkotARY>>>><>t. 09 201.99 0.0 218.79 142.00 -17.56 -218.09 0.0 218.79 48.80 lid.03 0.0 125.88 142.00 -10.55 -125.aa 0.0 125.88 14.00 37.87 0.0 41.11 142.00 -3.52 -Q0.96 0.0 41.11 TOTAL 443.73 1445.40 0.0 1774.29 -122.78 -1769.97 0.0 1774.29
<<<<a DRAG LOAD SLMIARY <<<<<<
DRAG LOADS PARALLEL 10 THE SEQIEHT AXIS tLBF)
CARTESIAN COORDINATES CYLINDRICAL COORDIHATES SEG)IENT Sl:QIENT t)Ut tBER X Y RESS. TANT AttGLEt DEG) RADIAL TANGENTIAL VERTICAL RESlATAHT TOTAL
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<<<<>> DRAG LOAD SNRIARY <<<<<<
DRAG LOADS NORNAI. TO T)IK 5EGHEHT AXIS tLBF)
CARTESIAN COORD IHATKS CYLINDRICAL COORDIHATES SKGHKHT SEGNEHT NNR)KR X Y Z RE5ULTAHT ANGLE I BEG) RADIAL TAHGENTIAL VERTICAL RESULTANT 379.87 291.66 855. lt d47.17 0.0 0.0 935.70 709.46 162.00 162.00 97.02 77.39
-930.66
-705.63 0.0 0.0 935.70 709.86 210.14 4dl.44 0.0 507.03 162.00 -57.Zd -503.79 0.0 507.03 141.35 308.37 0.0 339.22 16Z.OO -39.13 -336.9d 0.0 339.22 81.5d 177.Z1 0~0 195. 08 162.00 -22.81 -193.74 0.0 195.08 Zd.67 57.8Z 0~0 63.d8 162.00 -7.50 -d3.23 0.0 63.68 TOTAL 1131.Z4 2507.14 0 0 2750.57 -301.12 -2734.00 0.0 2750.57 I
<<<<<<DRAG LOAD SIR)NARY s>>>>
DRAG LOADS PARALLEL TO TNK SEGHEtIT CARTESIAN COORDINATE5 AXI5 (LBF)
CYLIHDRICAL COORDINATES gC'Q+r SKGHKNT SEGIIENT NIPIBER X Y Z RESULTANT ANGLKIDKG) RADIAL TANGKHTIAL VERTICAL REMA.TANT 1 b
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<<<<<< DRAB LOAD SU)%fARY <<>>>>
DRAG LOADS HORHAL TO THE SKGHENT AXIS fLDF)
CARTESIAN COORDIHATKS CYLINDRICAL COORDINATES SKB)fKHT SEG)fEHT
)A)ffdER X Y Z RESULTANT AffGLEfDEG) RADIAL TANGENTIAL VERTICAL RESULTANT 1 td7.d5 d52.71 0.0 705.45 ldt-00 -52.85 -703.47 0.0 705.45 t 20d.'3l 493.72 0.0 535.09 162.00 43.64 -533.31 0.0 535.09 l49.57 351>74 OoO 382.22 162.00 -33.55 -380.74 0.0 302.22 4 101.17 2'34.93 0.0 t55.79 162.00 -23.dt -254.70 0.0 255.79 5 58.dO 134.99 0.0 147.16 ld2.00 14.02 -146.49 0.0 147.16 6 19.20 44.05 0.0 48. 05 ld2.00 -4.d4 -47.83 0.0 48.05 TOTAL '0t.49 19lt.14 0.0 t073 ~ 7d -172.32 -20dd.54 0.0 2073.76
<<>><<DRAB LOAD SitfARY <<<<>>
DRAB LOADS PARALLEL TO THE SEG)IEHT AXIS tLBF)
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<<<<<<C.O. LOAD 6( DNRCNIKR 4 PX-d0052-2,RN( 12,17-21 SKC. PAGE
<<<<<< DRAB LOAD SUtOIARY <<<<<<
DRAB LOADS N(AXIAL TO THE SEQIEHT AXIS (LbF)
CARTESIAN COOROINATKS CYLIN)R ICAL C(XROIHATES SKBNEHT SEGHKNT
)<<A(bER X Y 2 RES(X.TANT ANGLE(DEG) RADIAL TANGENTIAL VERTICAL RES(X.TANT 1 104'1 1039.87 0.0 1045.05 ie0.00 104.01 1039.87 0.0 1045.05 2 56.7d 781.71 0.0 783.77 180.00 5d.77 -781. 71 0.0 783.77 3 24.95 554.83 Owe 555.39 180.00 24.95 -554.83 0.0 555.39 4 >>9.15 370.35 0.0 370.46 180.00 9.15 -370.34 0.0 370.46 5 ~2.64 212.98 0.0 213.00 180.00 2.d4 212.98 0.0 213.00 6 0.46 d9.5d 0.0 d9.56 180.00 0.4d -d9.56 0.0 69.56 TOTAL 197.97 3029.29 Oi0 3037.23 197.98 -3029.29 0.0 3037.22
<<<<<< DRAB LOAD SNOIARY <<<<<<
DRAB LOADS PARALLEL TO THE SEQIENT AXIS (LSF)
CARTKSIAN COOROIHATKS CYLINDRICAL COORDINATES SEQIENT Y Z RES(LTAHT ANGLE(OEG) RADIAL TANGENTIAL VERTICAL RES(LTANT
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a<<IC.O. LOAD OH Doe)CDHKR+PX4005t-t,let 12,17-21 SKC. Nll PAGK
<<Ia DRAB LOAD 5%0!ARY a>>a DRAS LOADS teRNAL TO T)tK SEGHKNT AXIS tLSF)
CARTESIAN CODROINATKS CYLINDRICAL COORDINATES SKBHKHT 3KGHENT tA)tR) ER X Y Z RKSULTANT At)GLE) DEB) RADIAL TANGKNTIAL VKRTICAL RESULTANT 1 47.31 1046.00 0.0 1047.07 180.00 -47o30 1046.00 0.0 1047.07 lb.95 78'9. 01 0.0 790.07 180.00 -40.94 -789.01 0.0 790.07 32.62 Sdl.19 0.0 5dZ.14 180.00 32.d2 -561.19 0.0 5dZ.14 23.35 374 '4 0.0 0.0 375.47 180. 00 -23.35
-13.90 374.74
-215.41 0.0 375.47 5 13.90 215.41 215.86 180.00 0.0 215.86 d 4.61 70.3Z 0.0 70.47 180.00 -4.dl -70.32 0.0 70.47 162.74 305d.db 0.0 30dl.08 -ldt.73 -305d.db 0.0 30dl.08
<<wa DRAG LOAD SUtttARY ass DRAB LOADS PARALLEL TO THK SEGHENT AXIS tLSF)
CARTKSIAN COORDINATES CYLINDRICAL COORDINATKS 5 KOHEN'leKR SEGHENT X Y Z RESS.TANT ANGLElDEB) RADIAL TANGENTIAL VERTICAL RESiA.TANT
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<<>>>>C.O. LOAD ON DOtCNER 843 PX-40052 2 6RtN 12617-Rl SEC. PA6f
<<<<<<DRAC LOAD SQItARY <<<<>>
ORAQ LOAD5 NORHAL TO THE SKGHENT AXIS tLSF)
CARTKSIAN COORDINATES CYLINDRICAL COORDINATES SKGHENT 5EGHKNT tAA)SER X Y 2 RESLLTANT ANGLE(DEC) RADIAL TANGENTIAL VERTICAL RESLLTANT 1 39R.RR 10R4674 0.0 1091.25 142.00 -5d.34 -1095.80 0.0 1097.R5 R '303.41 774629 060 831.4R 142. 00 -49.28 830.14 0.0 831.dR R21. 18 550.95 0.0 593.49 142.00 -40.10 59R.33 0.0 593.49 4 150.35 347.44 0.0 397621 142.00 -29.37 -394. 1R 0.0 397.21 5 81.35 Rll. 14 0.0 RR8.50 142.00 -11.83 -227.80 0.0 2R8.50 4 28.44 d8.89 0.0 74641 142.00 -5.91 -74.37 0.0 74.41 TOTAL 1183. 17 R991.49 0.0 3222.88 -198.91 -3R14.59 0.0 322R.88
<<>><<DRAG LOAD SLAOQRY <<>>>>
DRAC LOADS PARALLEL TO THE SKCNENT AXIS (LSF)
CARTKSIAN CQX)DINATE5 CYLIteRICAL COOROIHATES SKGHKNT SEC) IENT tAAI)ER X Y Z RESLLTANT ANGLE(DEC) RADIAL TAHiENTIAL VERTICAL REStLTANT Al ~
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DRAG LOAD5 NORIIAL TO THE SEGHENT AXI5 ILOF)
CARTKSIAN COORDINATES CYLINDRICAL COORDINATES SEGHENT SEGHENT tARR)ER X T 2 RESISTANT ANGLE(OEQ) RADIAL TANGENTIAL VERTICAL RESILTANT 1 434.94 407.Rb 0~0 744.90 143. 00 10.10 -744. 74 0.0 744.90 2 343. 0'3 500.32 0.0 425.11 143.00 15 ~ 35 424.92 0.0 425.11 3 203.05 391 ~ 79 0.0 403.34 143.00 9.73 -403.25 0.0 403.34 4 R00.44 274 '4 0~0 3'79 143.00 5.02 339.75 0.0 339.79 5 119. 15 141 70 0.0 200.05 143.00 2.15 R00.04 0.0 200.05 4 39.49 53.35 0.0 44.30 143.00 4.57 44.37 0~4 44.30 TOTAL 1440.94 1994.00 0.0 2442.45 50.93 -2441 90 0.0 2442.45 kJ I
0
<<<<<<ORAQ LOAD SNOIARY <<<<<<
0+1 ORAQ LOADS PARALLEL TO THK SEGHENT AXIS (LBF) 1>
CARTESIAN COORDINATES CYLltE)RICAL COOROINATE5 ?'.
SEQIIEtiT SEG)IENT 4 tA)tE) ER X T Z RESLLTAHT AHGLEIOEG) RADIAL TANGENTIAL VERTICAL RESLLTANT n
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<<raC.O. LOAD OH DOWCOHER 0103 PX-4005t-t,Rlkl 12,11-21 SEC. rrr PAGE rrr DRAG LOAD Slk0lARY <<rr DRAB LOADS NORNAL TO THE SKGNENT AXIS lLbF)
CARTE5IAH COORDINATES CYLI)E)RICAL COORDINATES SKBHKHT SKBNKNT MASER X Y 7 R ESN. TANT ANGLE(DKB) RADIAL TANGKNTIAL VKRTICAL RESU.TANT 1 406.49 551 o9t 0.0 d65.57 139.50 4'9 .19 463.61 0.0 665.51 t 345.d5 454.14 0.0 571.19 139.50 32.50 -570.26 0.0 571.19 271+52 346.95 0.0 442.14 139.50 20.16 441.46 0.0 442. 14 193.32 244+79 0.0 311.92 139. 50 11.96 -311. d9 0.0 311.92 5 115. 27 144.4d 0.0 164.91 139.50 4.30 -164.66 0.0 184.97 d lb.td 47o61 0.0 dl.23 139.50 1.95 dl,20 0.0 61.23 TOTAL 1310.7t 1792.6d 0.0 2251.04 122.01 -2253.51 0.0 2251. 03
<<rr DRAB LOAD SEMINARY rrr DRAB LOADS PARALLEL TO THE SEG)tENT AXIS (LDF)
CARTKSIAH COORDINATES CYLI)E)RICAL COORDINATES SKG))KHT SEGNKNT HLER)ER X Y Z RESS.TANT ANGLE I DEB) RADIAL TANGEHTIAL VERTICAL RESN.TANT
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<<aa DRAG LOAD SLRtLARY aaa ORAQ LOlDS tCIHAL TO THE SEGHENT AXIS ILbf I CARTESIAN COMDINATES CYLINDRICAL COORDINATKS ANGLE(DEGAS SEGHENT SEGHENT NAKER X Y Z RKSLLTANT RADIAL TANGENTIAL VERTICAL RESLLTANT 1 459.59 500.00 D.O 4R7.49 305.00 -31. 25 427.10 0.0 827.49 2 549.1t 403 '9 0.0 48).31 305 F 00 -15.39
-5.72 481.)3 0.0 0.0 481.31 421.83 302.34 0.0 519. 00 305 00 518.97 519. 00 294.89 R08.31 0.0 341.04 305+00 -1.50 341.04 0~0 361 04 5 173.45 121.70 0.0 tlt.05 305.00 0.09 e)2.05 0.0 212.05 4 57.t7 40.00 0.0 49.84 305 F 00 0 08 49.86 0.0 49.86 TOTAL t) 54.34 )S7$ .44 Oo0 R470.94 53.88 2470.14 0.0 2470.94 aaa DRAG LOAD SQtllRT aaa DRAG LOlDS PARALLEL TO THK 5KGHENT AXIS (LOF I CARTE5IAN COORDINATES CYLINDRICAL COORDINATE5 5EGHENT 5EGHENT tlASER X Y 2 RKRLTANT ANGLE(DEG) RADIAL TANiENTIAL VERTICAL RESLLTANT 1 ':. i, (
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<<<<<<DRAb LOAD SIKRIARY <<<<>>
DRAG LOADS NORHAL TO THK SEG)IENT AXI5 ILDI')
CARTESIAN COND IHATES CYLINDRICAL COORDINATES SKGHENT SKGHENT tk<<SER X Y Z RKSLLTANT AtSLEIOEG) RADIAL TAtSENTIAL VERTICAL RESISTANT 1 547.98 520.48 O.D 755.74 337.50 307.08 490.54 0.0 755.76 e 404.35 453.99 0.0 407.95 337.50 199. 83 574. 17 0.0 407.95 279.79 3d4 31 0.0 159.35 337.50 119. 08 443.45 0.0 459.35 4 182.97 Rdt.43 0.0 3RO.Ob 337.50 48.53 312.d6 0.0 320 F 08 5 103.87 157.54 0.0 188.72 337.50 35.47 185.31 0.0 188. 7R 4 33.72 52.1R 0.0 42.33 337.50 11.09 41.34 0.0 4t.33 TOTAL 155R.47 lbll 30 ~ ob t391.19 741.29 R247.49 0.0 R394.19
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<<<<<<ORAQ LOAD SQOQRY <<>>>>
DRAG LOADS PARALLEL TO THK SE6HENT AXI5 (LSF)
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CARTESIAN COORDIHATKS RESULTANT CYLIIIRICALCON)DIHATES SECkfKNT Y Z ANGLE(OEB) RADIAL TAtOENTIAL VERTICAL RE%@TANT 1 453.4t 348.td 0.0 571.89 139.50 -118.74 -559.43 0.0 571.89 t 340.to 317+04 0.0 479.8d 139.50 47.98 475.03 0.0 479.84 t48.78 t43.5t 0.0 37d.4t 139.50 -33.84 374,95 0.0 374.4t 185'4 194.41 0+0 t48+94 139 '0 -15.05 K48.5t 0.0 K48.94 5 109.19 118. K4 0.0 ld0.94 139.50 . -4.24 -140.8t 0.0 140.94 d 34.03 39.59 0+0 53.53 139.50 -1.48 -53.50 0.0 53.53 TOTAL 1413.44 lt81.08 D.O 1911.59 -t4Z.95 -189K.t4 0.0 1911.58
<<<<<<DRAB LOAD SNOlART <<<<<<
DRAB LOADS PARALLEL TO THE SEGHENT AXIS (LBF)
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1.000000-02 -1. 7756E-03 .34931 1 3271E 02 1.10000D-OR R. 1493K-03 .39803 1 ~ 512 ZE 02 1 ~ ROOOOD OR R.5493E-03 o 40190 1 5269E 02 1.30000D 02 -2.965SE-03 .43120 -l. 638" E-OZ 1.400000-02 3.4058E-03 .44881 -l. 7051E-02 1.50000D-OR 3.8860E-03 .51159 -1.9436 E-02 1.600000-02 4. 4121E-03 .54059 -R.0538E-OR 1.700000-02 4.9d02K-03 .55554 2.1106E 02 1.800000-02 5.5363K-03 .59674 -2 ~ 2d 71E-02 1.90000D-OR -6. 1541E-03 .d3S90 R.4273E-OR 2.00000D-02 d.8067K-03 .6d625 2.5314E-OR 2.100000-02 7.4780K-03 -.d7d'39 -Z.56'97E-OZ 2.200000-02 -8.1671K-03 .70173 -Z.d660E-02 2.300000-02 -8. 8721E-03 .70834 -2.6911E-OZ 2.40000D OR -9. 5921E-03 -.73171 -2.7799E-OR 2.500000-02 -l. 0335K-02 -.75448 -2.8664E-OZ 2.60000D-02 -1. 1101K-02 -'.77670 -2 '508K-02 Z.700000-OR 1. 1910E-02 -.84097 -3.1950K-OZ 2.800000-02 -1. 2740E-02 -.81936 -3. 1129K-02 2.90000D-02 -l. 3581E-02 -.86274 -3.2777K-OR 3.000000-0R -1. 4 430 E -0 Z -.83605 -3. 1763E-02
'3. 100000-02 -1.5Z76E-02 -.85461 -3.2468E-02
.3.20000D-OR -1.6152E-02 -.89785 -'3.4111E-OR 3.300000-02 -1.7072K-02 -.94215 -3.5794E-OR 3.400000-02 -1.8037E-OZ .98745 -3. 7515E-02
'.:: 3+50000D-02
~'3I60000D!OR 5;~000dDrOR 1.9033E-OR 2.0049E-02 Z. 1067E-02 1.0061
-l. 0243
-1.0127
-3.82Z5E-OR
-3.8915E-OZ
-3.8473K-02 r'0 Q48h-ot- R.ROSSE-OR .96892 -3. d811E-02 r:.) "g'3 j90ODCD<oei R.3034E-OR -.98308 -3.7349E-02 ir4')4QOOtlDLoe:. 2.3976E-02 .90199 3.42dBE-02
',~'i >;"'. 2.4900E-OZ -.94508 3.5905K-OR IIIi40ya1]OC'".I 2.5834E-OR -.92291 -3.50d3K-OZ
'~,'~3000)P ddt; 2.6813K 02 1.0345 -3.9301K-OR
- .',;; <<pobobD;Ot, 2.7905E-02 1.1503 -4.3700E-02
..;: '.4,$ 00000~0) 2.9080K-OZ -1.1992 -4.5559K-OR
'..'g:%edoODOD<oh 3.0304E-02 -1. 2492 -4.7459K-02
'I'toOOOD~OR 3.1597E-OZ -1.3374 -5.0809E-02
.. 4".80000D-Oe 3.2942K-OR -1.3524 -5. 1381K-02
;, q.90OOOD-OR -3.426'3E-02 -1. R896 -4.8993E-OR
<r Q~OOSOOD OR -3.5519K OZ -1.2231 -4.6467E-OR
~ ~
g IXI
r'I 4
rD DE.
1+
lrg Va ter Dr I
J,
5 bKKH APPRDXIHATKO bY A RECTANGLE TANGENT TO THE HALLS. ON.
THE .IZK IS R0.250 RO.R50 25.000 TINE>> 1.00 bUbbLK DOWCD) IlKR SOURCK SDURCE SOOT RADIAL ANGULAR AXIAL DRAHING INDEX I)K)KX RADIUS STRENGTH LOCATION LOCATION LOCATION ANGLE 1 ~ >> <'ha e 1 ~ 000 5.835 54.t7 7+000 3.142 13.000 0.0 t t 1 ~ 000 2.185 49.51 7.000 2;356 13.000 45.000 3 I+000 2<<185 49o31 7.000 1.571 15.000 90.000 1.000 2 ~ 185 49.31 7.000 0.765 15.ono 135.000 5 5 1 F 000 t.185 49,31 7+000 0.0 13 ~ 000 180 F 000 4 4 l<<000 5.833 54.27 7.000 5.498 13.000 225.000 7 7 1 000 5.833 <<54.27 7.000 4.712 13.060 210.000 8 1 ~ 000 5.853 54.27 7.000 3.927 13.000 315.000
<<<<>><<<<<<<<>><<VELOCITIES A)O ACCKLERATIDHS AT OEDHETRIC CENTERS DF 5EGHENTS AT TINE>> 1.000 SECONDS <<>>>>>>>>>>>>v>>
VKLDCITYlFT/SKC) ACCELERATIDN(FT/SEC<<>>R )
SKOHKNT HO ~ Y Z RK5ULTANT X Y Z RKSULTANT 1 0.'Rl 0<<37 0<<30 0.5R 2.76 -4.72 15.41 14.48 t 0.14 -D.R7 0.18 0.37 2 F 08 5.52 3.55 5.41 1
0,
-Oo07 ll 0.19
<<0 ~ lt 0 ~ 30 0.34 0.37 0.37 1.4d 0.96 2.42
<<1.56 1.58 0.64 3.24 R.OR 5 -o.o4 0.07 0.37 0.37 0.55 <<o.e7 0.50 1. 14 booed rir ~wr 0~4'I- s )
4 0,01 0.02 Oo37 0,38 0.18 0.28 0+35 0.49
<<<<<<<<>><<<<>><<VELOCITIES AHD ACCELKRATIDNS NDRHAL TO SEGHENT AT TItlE
- 1.000 SECONDS <<>>>>>>>>>>>>>>>>
HDRHAL VELOCITYlFT/SKC) HDRHAL ACCELERATION(FT/SEC>>>>2)
SKSHENT HO. Y Z RESULTANT X Y Z RESULTaNT 0.21 0.37 0,0 o.42 <<2.7d -4.7R 0~0 5.4d
<<0 ~ 16 -oo27 0 ~0 0.3R 2.08 3.52 0.0 4 F 08 0.11 -0.19 0~0 0.22 1 ~ 46 2.42 0.0 2.85 dt's 0.01 0o lR Ooo 0.14 0.96 1.56 0.0 1 ~ 85
<<Oo04 <<0 ~ 01 OIO OaO ~ O.SS <<Oi81 'OeO le0$
<<O.ol o,ot 0~0 0 F 05 Solo MRS 0.0 0 '3
<<<<<<<<<<<<<<<<<<ORMS AT TIHK <<1 000 SKCDHDS <<>>>>>>>><<<<>><<
VELOCITY DRAG lLBF) ACCELERATIDN DRAG lLBF) TOTAL DRAG lLBF)
SKQHENT $4 ~ ' Y Z R KSULTAHT X Y Z R E5ULTANT Y Z RESLL']ANT 0,44 0 ~ 81 0.0 0.93 <<71.52 121.96 0.0 141.28 7).79 122.77 0.0 142.22 O,t4 0.45 0 0 0.52 53.67 90.94 0.0 105.40 -53.94 91.59 0.0 104 12 0 ~ 13 0. Rl 0+0 0 F 25 37.73 d2.59 0.0 73 ~ 09 37 ~ 86 81 n.o 75.34 0.05 0 F 09 0.0 0.10 24.89 -40.35 0 ' 47.41 24.94 <<40o44 0.0 47 '1 ooot oo03 0~0 0.03 -14.17 22.59 0.0 Rd.d7 14. 19
-4,dl
<<Rt.dt 0.0 26 '0 oooo oooo 0 ' 0+00 4odl 7.20 0.0 S.dl 7.28 0.0 8.61 TOTAL 0<<93 -1,59 0.0 1 ~ 84 20d,40 545.71 0.0 402od5 -207.35 -347 ~ 30 n.o 404.50 SSS H-FACTORS AT TINK >> 1.000 SKCDNDS SSS 1 F 000 1 000 1.000 1.000 I+000 1.000 1.000 1.000 A
't
$ 1
+I 4
g!
r ~ bEEN APPROXIHATKD SY A RECTAHGLK TAHGKNT TO THK HALL; ~ OOL THAN K IS RO 250 t0.250 R5.000 TIHE<< 2 00 OVBSL<< DON)COttHER SOURCK SOURCK SDOT RADIAL . AHGVLAlt AXIAL DR AKING INDEX INDEX lkADIUS STRENGTH l.OCA7 ION LOCATION LOCATION AlIGLE 1 I ~'">> 1 ~ 000 2.850 52.51 1.000 3. 142 13 F 000 0.0 2 2 1.000 0.951 50.01 7 ~ 000 . 2.356 13.000 45 F 000 3 li000 0.951 50.01 7.000 1.5'll 13.000 90.000 4 . 1.000 0.951 50.01 7.000 0. 785 13 ~ 000 135.000 5 5 1 F000 0 ~ 951 50.01 7.000 0.0 13.000 180.000 6 6 lo000 >>Zo850 52.51 7.000 5.498 13.000 RZ5.000 7 7 1.000 Ro850 -5R.51 7 000 4.712 13.000 210.000 8 8 1.000 2+850 5R,51 7.000 3.9R7 13. 000 315 F 000
<<<<<<<<<<<<<<<<<<VELOCITIES Ate ACCKLKRATIDHS AT GEDHETRIC CEHTERS OF SEG)IEHTS AT TI)lE e t.000 SECO)CS <<wwwmaaaw SKG)kKNT NO+
VELOCITY(FT/SEC)
Y Z RESULTANT X ACCELERATIDNlFT/SEC<<<<2)
Y Z RESULTANT cAL..'g. !>I77. p$ -pp(- $ o8a 2 1 >>0.10 0.17 0+II 0. 23 2.73 4.d7 1'3.81 14.83 2 0.08 -0.13 Doll 0.19 -2.06 3.48 3.85 5.58 0 ~ 05 0.09 0 ld
~ 0.19 -1.44 R.40 1.81 3.37 0 ~ 04 0.06 0.18 O.ZO 0.95 '.54 1.13 2+14 5
6 Oo02 0.01
-0.03 0.01 Oe19
-0.20 0.20 O.RO
<<0.54 0.18
-0.86 0.28 0.79 0.65 1.29 0.73 Jn'Vzcn~~oy r ')
N
<<<<<<<<<<<<<<<<<<VELOCITIES AHD ACCELKRATIDNS HORtlAL TO SEOHEHT AT TItlE s 2 ~ OOO SECDteS <<xevaaxww NORHAL VKLOCITYlFT/SKC) HORHAL ACCELERATIDNlFT/SEC<<>>2)
Y Z RESULTANT X Y ' RESULTANT N
1 -0.10 0 17 0.0 0.20 -RE 73 4.d7 0.0 5.41 t 0 F 08
~0 F 05 0 ~ 13
-0 '9 0.0 0,0 0 '5 0.10 2 '6
-1 44 3,4S R.40 0.0 0.0 4.04 2.80 4 -0 04 0.06 0.0 0 '7 0.95 0.54 1.54 0.86 0.0 1.81 b 5 0.02 0.03 0~0 0.04 . 0.0 1.0Z 6 -0.01 -0.01 0.0 0.01 -0 ~ 18 MRS 0.0 0.33 R t
<<<<<<<<<<awe<<DRAGS AT TIKE s 2.000 SECONDS <<wa<<<<saw<<
b
',c VELDCITY DRAG (LOF) ACCELERATION DRAG lLOF) TOTAL, DRAG lLBF)
SNHSP ten" ' Y Z RESUl.TAHT X Y Z RESULTANT Y Z RESUl.TANT 1 F 10 -0.18 0.0 0.21 70.65 120.64 0.0 139.81 -70.15 -120a83 0.0 140.02 2 0.06 <<0. 10 0.0 0.12 53.15 89.91 0.0 104.50 -53.20 -90.08 0 ' 104.62 3 0 F 03 0 ~ 05 0 ' 0.06 -37.3d <<dl.94 0~0 72.33 31,39 -61.98 0.0 7Z.39 4 -0.01 0,00 0 '2
-0.01 0.0 0.0 0.02 24.64
- 14. 03 39.93 22.35 0 ~0 0.0 46.92 2d.39
> n< v> p y- - > J. > < <<rrrr>>>>rr VELOCITIKS ANO ACCKLERATIOH5 HORHAL TO 5KGHENT AT TIHK s 3.000 SECOteS>>>>>>>>>>>>>>>>>> NOR)tAL VELOCITY(FT/SEC) NORttAL ACCELERATION(FT/SEC>>>>2) SEGHKNT HO0 X Y Z RESULTANT X Y Z R E5ULTAHT 1 0.14 0.0 0.28 40d3 <<7.92 0.0 9.11 ~V t 0 ~ 10 0.0 0.21 3.48 5.90 0~0 6.85 -0.07 0.0 0 ~ 14 R045 4,06 0~0 4.74 0.05 '3 0.0 0.0 0 '9 l,dR 'R.d2 0~0 '0 ~ 0 F 08 5 . <<0 i .0 <<0.01 0.0 0 F 0.02 05 0.92 0030 1.41 0 47 ~ 000 1.73 0 ~ 56 1 ~'0 t ~ i: ;Qr0 AT 5.000 50CCIDA <<0 ~ I0<<00 0;;i.A j1 0150 ~ b 0 ~ .T ig ~ VELOCITY ORAB tLbF) ACCELERATION ORAB tLbF) TOTAL ORAG tLSF) I Y Z RESLLTANT X Y Z RESULTAHT Y Z RESULTANT 0034 0.0 0040 119,71 204.68 0.0 237 ~ 12 -119.91 205.02 0.0 237.52 1 -0. 19 0.0 O.RR 90.08 152.6R 0.0 111. RZ 90 F 20 -152.81 0.0 177.44 . 'I I $ ~, lf!4'0 ~ 05 0 '9 0.0 0.11 d3033 105. 05 0.0 12R.dd -d3,39 -105.14 0.0 122. 71 '7 '2 0 I CA"0I 0 0.04 0.0 0.04 -41 67 0.0 19.57 -41.00 -67.1d 0.0 79.61 I 0.01 0.00 0.0 0.0 0.01 -23.79 -37.92 -12. Rl 0.0 0.0 44.7d -23 '9 -37.93 0.0 44.77 0 F 00 7013 14 45 7 ~ 73 -1Z.21 0.0 14.45 .'."TOTAL,'j ':,i'i 1.40 O.d7 0.0 0 78 -346 '2 580.20 0.0 675.79 -346.82 580.S7 0.0 67d.57 ' 488 H+FA+NIS'AT TIHK>> 3.000 Oil ~ i' 000 1.000 1.000 SECONDS 1.000 1.000 1.000 1.000 1.000 (ly 0.0) 'P% g 'I I 44 i<I j!l C4 l4 foal,'~ 4p X% 51 4L 4 la ~P 't )i. AS O'EEN APPROXIHATKD BY A RKCTAHGLE TANGENT TO THK HALL'OOL TH. IZE IS t0.250 RO.R50 25.000 TIHKa 4.00 BIA)BLK OO)t)CO)OIEk SOURCK SOURCE SOOT RADIAL AHGULAR AXIAL ORAHING INDEX I)OKX RADIUS STREHGTH LOCATION LOCATION LOCATION AHGI.E 1 t<'tt)NI t 1.000 -2 '15 9d.80 7+000 , 3.142 13.000 0.0 R e 1.000 R5.325 285.54 7 F 000 2.35d lb.000 45a000 3 1.000 25.325 285+54 F 000 1.571 13.000 90.000 4 4 1+000 25,325 285.54 7.000 0.785 13.000 135.000 5 5 1.000 R5.325 285.54 7.000 0.0 13. 000 100 F 000 4 4 1+000 2+515 96.60 7.000 5.496 13.000 2"5.000 7 7 1.000 2.515 96.80 F 000 4.712 13.000 270.000 8 6 lo000 2+515 96.80 7.000 3+927 13.000 315+000 <<aaaaaaaa VKLOCITIKS AHD ACCKLKRATIONS AT OENIETRIC CENTERS OF SEGHEHTS AT TIIIE>> 4.000 SECONDS a>>a>>>>>>>>>>a VELOCITY(FT/SEC) ACCELKRATIONIFT/SEC>>>>2) SEGHEHT NOt Y Z RESULTANT X Y Z RESULTANT C/-", I/O / (77 I~/ PX d g . I 0.74 -1.24 9,03 9el5 10.3b 17.21 94.0R 98. 10 2 0.57 0 40 0 94 0.45 4.33 3.52 4,47 3.40 7o75 5.43 12.90 -8.90 42.07 32.34 44.db 33.9S ( C 0. L owrI g~ 'Or rt r4.~0 4 -Ootd 0.42 3.24 3.27 3.56 5.73 28.93 R9.71 5 4 "0+15 <<Oo05 0.23 0 07 3.12 3+07 3.13 3+07 RE 0.4d 04 3.21 1.03 27.41 c.dt79 R7.67 Rd.62 'one ~orget.o--,( >Z ) <<a<<aaaaa<<VKLOCITIKS A)e ACCELERATIONS NORHAL TO SEG)IKNT AT TIHE a 4.000 SECON)5 a>>a>>>>>>>>aa NORHAL VKLOCITYlFT/SKC) NORHAL ACCKLERATIONIFT/SEC>>>>2) SEGHKNT NO+ X Y Z. RESULTAHT X Y Z RESULTANT 1 0.74 l.t4 0.0 1+46 10,36 17.21 0.0 R0.10 I ~ e -0.57 0 ~ 94 0~0 1 ~ 09 7.75 12.90 0.0 15.04 0 F 40 0.45 0~0 0 74 5.43 -8.90 0.0 10.42 4 O.Rd 0.42 0~0 0.49 3.5S 5.73 , 0.0 d.7d 5 0.15 ~0.23 0~0 Ootb -2 04 F -3.21 0.0 3.80 4 Oo05 0.07 0 ' 0 ~ 09 -0.46 1.03 0 ' 1.23 ) TIHK << 4.000 SECONDS <<aaaaaaaa I tlfj'i. VKLOCITY DRAG lLBF) Y Z RKSULTANT X, ACCELERATION DRAG.(LBF) Y Z R ESUL TANT TOTAL DRAG Y ILBF) Z RKSULTANT ')jtoS+60 9.44 0.0 ~ 11,06 Rdb.32 445.12 0.0 519.74 -274 12 F -454.56 0.0 530.62 t)i3.t3 5. 3g OoO d.RR ROO.RS -333. tI8 0.0 '389.00 -203.51 338.80 0.0 395.22 'l) . ( It (~(l It;t .g. I /I, " > . I 56 2.54 1.06 0~0 0 ' ~ 2.99-141.05 -93.2R 232.56 149.31 0.0 0.0 272 '1 176+03 0.33 0' 0.40 52 'd 82.94 0.0 98.30 -52.98 -83.27 0.0 90.d9 0.03 0~0 0.04 17.1d 24.70 0.0 31.74 -17.18 -26 F 73 0~0 31.76 16.74 0~0 el+98 -771.37 -1266.51 0.0 1482.97 -7S2.86 -1205.24 0.0 1504.95 K tt F 000 SECONDS 8<<8 1 F 000 1.000 1 F 000 la000 1.000 1.000 1.000 Zj 4'y ~l~ I '1 f~ HAS BEEN APPROXINATKD BY A RECTANGLK TANGENT TO TNK NAL. E POOL SIZK IS RO ~ R50 20+250 25.000 TINE>> 5.00 BUBBLE DO)6)COWER SOURCE SOURCK SDOT RADIAL ANGULAR AXIAL ORANING INDEX I)SEX . RADIUS STRENGTH LOCATION LOCATION LOCATION ANGLE 1 Iel il gylf ~ 1.000 -13 ~ 095 -304.37 7.000 3. 142 13.000 0 ' R 2 1 F000 11.576 2R3.39 7.000 t.35d 13.000 45.000 3 1.000 11.51d 223.39 7.000 1.571 13.000 90.000 1 F 000 11.574 223.39 7.000 0 ~ 785 13.000 135.000 5 5 1+000 11.51d 223.39 7.000 0.0 13.000 100 F 000 4 4 li000 13.095 304.37 7.000 5.49S 13.000 225.000 7 7 li000 13.095 304.37 7.000 4 '1R 13. 000 210. 000 8 1+000 <<13 +095 -304.31 7.000 3.927 13.000 315.000 aaaaaa>>aa VELOCITIES A)O ACCKLKRATIONS AT OKO)IKTRIC CENTER5 OF SEGllEHTS AT TIHK>> 5.000 SECONDS <<>>>>>>>>>>>>>>>> SKOHENT HO VKLOCITYlFT/SKC) Y Z RKSULTAHT X ACCELFRATIONlFT/SKC>>>>2) Y Z RESULTAHT rsi, ,zoo. I>I77 ~ n> /x dao+ 1 2 0.44 0.49 lait <<Os64 3.12 0.60 3.38 1.24 14.00 10'5 R4.08 17.94 55.60 10.27 d2.37 23.21 C. g. Lgnfl Ow P*d>~++ 0.35 0.58 0.33 0.75 -7.42 12.34 0.92 14.43 4 O.R3 0.37 0.14 Oi44 4,90 7.9d -2.67 9 ~ 12 L'O>Ij 5 ~~ . 0.13 0.21 0.08 0.26 2.79 <<4 '6 -4.36 d.83 gfn,ga(g S p i ) Oo04 0.07 0.04 Oo09 0.91 1.44 5.06 5.34 N 1 a>><<aaaaaa VEI.OCITIKS AHO ACCKLKRATIOH5 HORHAI. TO 5EGHENT AT TINE a 5.000 SECONDS>>>>>>>>>>>>>>>>>> HORHAL VELOCITYlFT/SEC) HORHAL ACCELERATION(FT/SEC>>>>2) SECHEHT HO+ Y Z RESULTANT X Y Z. RESULTANT l 1 0.44 1.1R 0~0 1,30 14 F 00 24.08 0.0 27.66 2 0.49 -0.64 0 ' 0.97 10.55 17.94 0.0 R0.81 <<0.35 0 ~ 58 0.0 O.d7 7.42 1R.34 ~ 0.0 14.40 4 0.'R3 0.37 0.0 0.44 4.90 7.9d 0.0 9.34 5 0.13 -0.21 0.0 0.25 2.79 4.46 0.0 5.2d I 4 0.04 -0.01 0.0 ~ 0.08 -0.91 lo44 0~0 1.10 "I , i I
- 1. Rd 140'9 9R.55 R30.02 148.25 0.0 0.0 269.43 174.77
!"I.'g'i,ii.',"T'l j~'ELOCITY DRAG tLBF) ACCELERATION DRAG (LBF ) TOTAl. DRAG tLBF) Y Z RESULTANT X Y Z RESULTANT Y Z RESULTANT f 0.0 8.60 3dZ ~ 03 d22.73 0.0 7I<<0.31 3d6.47 -d30.32 0~0 129.11 0 ~ 0 4.91 272.88 <<463 -319.17 '0 0.0 0.0 536.20 372.4d -215,37 -193.20 -468.13 -321. 19 0.0 0.0 543.12 l i 0.0 R.35 191 ~ 98 374.S1 0 ' 0.99 126 ~ 63 <<205.76 0 0 241. dl 121.15 -20d.dl 0.0 <<42.d0 0.0 0.31 72 ~ 09 115. 22 0.0 135i91 12.25 115.49 0.0 13d 23 0.0 0 ~ 03 23,42 37,12 0~0 43.89 -23.44 37 F 14 0.0 43.92 ~,('Q P,:: I",,;t )",; 8.85 14.98 0,0 17,40 1049 F 02 -17d'3.6'9 0.0 205R.3S -1051 ~ 81 -1778 ~ 87 0.0 2069 '8 Iili'~'ITTiili ..m+>f.;, ~j g,~ i "' i'f)~"ac@'1 000 1 ~ 000 5.000 SECONOS 1 000 1 In 000 1 000 Ie000 I F 000 1.000 i'i ~ ~ I i . i i ~ ~, Pg li) ~ J, l d L 14 ' L S bKKN APPROX]HATED BY A RKCTANQLK TAHGEHT TO THK HALL OOL ZK IS R0.250 RO.R50 R5.000 TIHK>> 4.00 BUBBLK DOHNCDtblKR SOUR CK SOURCE SDOT RADIAL AHGULAR AXIAL DRAHING INDEX INDEX RAD]US STRENGTH' LOCATIOH LOCATION 2 l 0'">"E' 1.000 -13.157 F 000 3.]42 LOCAT]ON
- y'. i,
- <<aa<<II<<aal,'. 50AIS AT TIHE a 5.000 SECOM)5 <<aaaaaa>>a
<<aa<<aa<<aa VELOCITIES Ate ACCELKRATIOHS AT GEOtlETRIC CKNTERS OF SEGHENTS AT TIKE a d.000 SECOtZ)S <<>>>>>>>>>>>>>>>> SEGHEHT HO ~ VELOCITY( Y Z ) RKSlKTAHT X ACCECERATEON(ETIAECA~ EE Y Z RESULTANT '.:"I. f/0 I'IT7 ~ ~ EAT PX 1 >>0049 0.85 0.87 103] 13.0R 21.75 107.25 ))0.2] C . 0 L rl P~.I.C g~.~ 0 C e '4 ~ C 2 0.37 O.d3 0.32 0 F 80 9 ld.28 44.45 40.33 -0.24 0.44 -0.59 0 F 78 -d.bR )).ZR 32,92 35.44 0.17 0.28 -0070 0 ~ 77 4.50 -7.23 28.82 30.0d 5 0.]0 <<0. 16 0.75 0.78 RA57 4.05 2d.98 27.41 4 0003 OAOS 0.78 0 78 0.83 1030 26.23 R6.28 <<a<<a<<<<a>>a VELOCITIES AHO ACCELERATIONS HDR)lAL TO SKGHEHT AT TIHE>> d.000 SECONDS a>>>>>>>>aa>>a HORHAL VELOCITYtFT/SEC) NORtlAL ACCELERATIDNtFT/SEC>>>>2) SKGHEHT NOA X Y Z RESULTANT X Y Z RESULTANT Og 1 -0 ~ 49 -0.85 0.0 0.98 i]3.02 21075 0.0 R5.35 2 4, 5 '" EE 0.37 0.2d 0017 0.]0 -OAd3 0.44 0 F 28 -0.16 0 '5 0~0 0 ' 000 0.0 0.0 0 73 0.51 0.33 0 ~ 19 0.06 9.74 d.bR 4.50 2.57 0.83 16.28 11 22 -7.23 D'OR 4.05 1.30 0.0 OAO 0.0 ..0.0 0,0 lb.96 13.]3 8.52 4.79 ]055 l T TIHK a F 000 SECDtSS <<aaaaaaaa
- 13. 000 AtlGLE 0.0 2 10000 5.436 7.000 2.35d 13.000 45.000 10000 5,434 7A000 1.571 13.0no 90.000 10000 5.436 F 000 0.785 13.000 135.000 5 5 1.000 5.43d 70000 0.0 13.000 100.000 4 4 1.000 13.157 F 000 5.498 13.000 RR5.000 7 7 1.000 13.157 F 000 4.7]2 13.000 270.000 8 8 . 10000 ]57 13 7.000 3.927 1'3 F 000 3]5.000 FT/SEC
~'-,(.-,'( l ) . 54HCHVPOj l; I'.l,)t Y Z RESULTANT X Y Z RESULTANT Y Z RESULTAHT b 5.02 33d,dR 5d2.39 0.0 d55.44 -339.1] 5d6.75 0.0 d60.46 2.80 -251074 -420.87 0~0 490.41 -25].15 -423 Zb 0.0 493.21 l 1.34 176 48 290.]5 0.0 339 ~ 61 -]77 AD ]7 291.30 0.0 340.95 0.56 -116.43 107 0.0 RZ0.30 116 ~ 72 -]87.50 0.0 R.ZO ~ 86 0.18 -d6.35 104.d4 0.0 123.91 -d6.45 -104.79 0.0 124.nb A.4",'l 'T'ai ~. ".0,0] 0,02 0,0 0.02 R]058 33.d9 0.0 40001 21.58 -33070 0.0 40.0Z TEAL E'l '099 8057 0~0 9 92 9d9 ~ 20 1598.7d 0.0 1869.46 -974.19 1607.33 0.0 1879.58 bbb HjFACTORS AT TIHE ~ d0000 SECONDS lib ~ ~ .-) . 1 ~ 000 1.000 1.000 1.000 1.000 1.000 10000. 1.000 ,Q t yt ~ <" '4'1 I. t HA5 BEEN APPROXIHATEO BY A RECTAHGLK TAHGENT TO THE HALL . SIZE I5 Ro<250 20<250 R5.000 TINE>> 7.00 BUBbLK DOWCDk%IKR SOURCE SDURCK SOOT RADIAL ANGULAR AXIAL DRAHING INDKX INDKX RADIUS 5TRENGTH LOCATIDH LDCATIOH LOCATION ANGLE 1 1.000 11.374 259<45 7.000 3.142 13.000 0.0 t t 1.000 6.689 391.31 7.000 R <356 13.000 45<000 3 1 F 000 d.db9 391.31 7 F 000 1.571 13.000 90.000 4 1.000 6.d89 391.31 7.000 0.785 13.000 135.nnn 5 5 1.000 6<689 391.31 F 000 0.0 13. 000 lno.ooo 4 4 1.000 11<374 259.d5 7.000 5.498 13.0no 225.000 7 7 1.000 11.374 '259.d5 7.000 4 '1Z 13.000 .270 000 F b 8 1<000 11,374 R59.65 7.000 3 '27 13.000 315<000 aaaaaa<<aa VELOCITIES AHO ACCKLKRATIONS AT OEDHETRIC CENTKRS OF 5EGHEHTS AT TIIIE ~ 7.000 SECONDS <<>>>>>>>>>><<>>>> VELOCITY(FT/5KC ) ACCELERATIONIFT/SEC>>>>2) SKOHKNT Ho< Y Z RK5ULTANT X Y RESULTAHT 1 t 0.48 0<3d 0<83 0.41 1.48 0 F 08 1 ~ Td 0.72 17.49 13<11 29.49 22.03 120.86 45.08 125.63 51.86 C c ~ i~. L o/ 8 g~ f>> c<~ ~ < ~ '3 0 25 -0.42 ~ 0.21 o.54 -9.ZO 15.18 30 ~ 78 35.53 4 -0.17 0.33 0.46 -d.07 9.79 25.59 28.06 5 4 "-0<10 0<03 O.ZT <<0.15 0<05 0,39 0.41 0<43 0,41 -3.4d 1 12 5.48 1.7d 23.23 ZR.R7 24.1Z RR.3d I <)QP /'<(lii)~g pp ~) g ) aaaaaaa<<a VELOCITIES AND ACCELKRATIOHS HDRHAL TO 5KGNENT AT TINE < 7.000 SECOHDS <<<<>>>>>><<<<>>a HDR)IAL VELOCITY(FT/SEC) HDRNAL ACCELERATIDNIFT/SEC>>>>2) SKGHEHT HO. X Y Z RESULTANT X Y Z RESULTANT 1 <<0.48 -0.83 0.0 0.95 17<49 -'t9.49 0.0 34.ZO t 0<36 -0.41 -0.42 0~0 0.71 13. 11 -22.03 0.0 25.64 0.25 0~0 0,49 ~9.20 15.18 ~ 0.0 17 F 75 4 0.17 -O.RT 0<0 0.32 6 F 07 -9.79 0.0 11.51 5 0.10 0.15 0.0 0.18 3.4d 5.48 0 0 d.48 4 0<03 0<05 0.0 0.06 1<12 1.7d 0.0 R.09 aaaa<<<<aaa DRABS AT TIHK a 7.000 5ECDHOS a<<<<<<<<<<<<<<a ~ ~ VKLOCITY DRAB tLbF) ACCELERATION DRAG <LBF) TOTAL DRAG )LBF) I ~ SKBHKNT +qr'Iil < X ' Z R K5ULTANT X Y Z R ESULTANT Y Z 'ESUPANT ~ I;..' Q 1<t 0.0 . 73 -45t.ZO TdZ.46 0.0 806.47 -454.56 -Td6.5d 0.0 8')1. 20 . 0.0 t . d4 -339.01 5d9.76 0.0 d62.99 -340.34 572.04 0.0 665.d3 0~0 1.2d '3 237.93 392.55 '3 0.0 459.03 -238.58 393.d3 0.0 460 '9 < .<)< ~ I 0.0 0.0 0 0.17 15d <95 -253 0.0 0.0 R97.76 -157.23 -89.51 253.49 0.0 298 '9 89.4Z 141.d2 167.48 -141 ~ 76 0 ldT.d5 0.0 0.02 -29<07 -45.60 0.0 54<08 29 F 08 -45<dt n.o 54 '9 .TOTAL I P (,g ..M<73 -b.od 0.0 9.35 1304.57 Rld5.03 0. 0 2527. 81 -1309.30 -2173.09 0.0 2537.15 I I bbb H-FACTO)5 AT TIHK a 7.000 5KCDHO5 8%% I<. I <. ', ), '1<000 1 000 1<000 1 000 1 000 1.000 1.000 1.000 I ~ ~ < << yQ 1 PF WC Irk r tg C, .7I 'OOL ~ J~ AS bKEH APPROXlttATKD BY A RECTANGLE TAHGENT TO THE HALL SIZE IS R0.250 20.250 R5.000 TItlE* 8.00 bUbbLK DOtbtCO)SKR SOURCK SOURCE ~ SOOT RADIAL AHGULAlt AXIAL DRAHIHG INDEX INDEX RADIUS STRENGTH LOCATION LOCATION LOCATIOH ANGLE I tag 1 q' 1.000 7 922 202.13 7,000 3 '4Z 13.nnn 0.0 t 1.000 3,916 214.37 7.000 2 35d 13.000 45.000 3 1.000 3.916 216.37 7.000 l. 511 13. 000 90.000 ' I+000 3.916 216.37 7.000 0.705 13.000 135.000 5 5 1.000 3.91d 214.37 7.000 0~0 13.000 180.000 4 1 F 000 7.92R -zn2.13 7.000 5.498 13.000 225.000 7 7 1 F 000 7o922 -202.13 ,7+ 000 4.71R 13.000 270.000 8 8 1.000 7i922 202.13 1 F 000 3 9R7 13.000 315.000 <<aaaaaaaa VELOCITIES Ate ACCELERATIONS AT IKOHETRIC CENTERS OF SEGtlEHTS AT TIHE <<8.000 SECOHD5 a<<<<<<<<<<a<<a SE6HENT Nni X VELOCITY(FT/SEC) Y Z RK5ULTANT X ACCELERATIOH(FT/SEC<<<<2) Y Z RESULTA)IT CBi . M!) ~ /a/77. g g pg -$ e9gW lt 0.31 Oet4 Ool7 0.54 0.40 -0.28 ~ 0.74 0.08 0.26 0.98 0.47 0.41 11.18 8.40 -5.90 19.02 -14.19 9 '7 dlobb 19+12 lb.77 65.70 25.25 15.70 C C. o. L own'~ P Ai'+ I ~ l O.ll 0.18 -0.33 no39 3i89 -6.30 7.47 10.66 5 4 0,06 0.02 -0.10 0 03 0.37 -0.38 0.39 Oi38 2 ~ 22 0.72 3.53 1.14 d.24 S.d5 7.50 5.80 Jo VwcgMnQ I g) N aaaaaaaaa VELOCITIKS AHO ACCELKRATIONS NORltAL TO SEGHENT AT TIHE <<8.000 SECOHD5 a<<<<a<<<<<<<<a HORtlAL VELOCITYtFT/SEC) NORtlAL ACCELERATIOH(FT/SEC<<<<2) M SEQHENT NO+ X Y Z RESULTANT X Y Z RESULTAttT 0Q l -0.31 0.54 0~0 0.43 11.18 -19.02 0.0 22.nd <<no 24 na40 0~0 0,41 bo40 14. 19 0.0 14.49 0 ~ 11 Ootb 0~0 0.3t 5.90 9.17 . 0.0 11.42 O. 11 0 F 04 0 ~ lb <<nein 0~0 0,0 0.21 bolt 3 '9 Zott d.30 3.53 0.0 0.0 1.41 4+17 I 0+02 0 F 03 0.0 0.04 0.72 1.14 0.0 1.35 I 5 I ~, L <<aa>>aaaa>> DRAt)S AT TIHK a 8.000 SKCOHDS aaaa<<a<<aa SESHENT NO+ ' VELOCITY DRAG lLbF) Y Z RESULTANT X ACCELERATION DRAG Y Z (LBF) R ESULTAHT TOTAL DRAG Y (LBF) Z R ESULTAHT 1 1.01 1.76 0.0 t.03 -tb9 00 491+91 0.0 570.52 290.02 493. d1 n.n 51Z 55 2 , <<0.57 O.Rb ni98 0 47 0.0 1.1'3 0,54 F 217.21 -152.dt 367.04 'Z 0.0 0.0 426 '0 295.23 -217 '8 -152.90 -358 F 02 253.10 0.0 427.d3 0~0 252 0~0 295.17 4 0.1R 0 ~ 19 0.0 0.23 -100.67 162.91 0~0 191.51 <<lnno79 -163.10 0~0 191.74 5 no04 0.04 0~0 0.07 57 33 -91 ~ 20 0.0 107.13 -57.37 91 '6 0.0 107.80 4 ' F 00 0 F 01 an 0.01 lb.d3 29.37 0.0 34.78 -lb.44 -29 '8 s 0.0 34.79 TOTAL -2 F 03 -3.47 0.0 4.02 835.48 -1395.15 0~0 - 1626.27 -837.51 -1398,62 l 0.0 1630 'Rb Cti K-FACTORS AT TltlE <<8.000 SCCOtQS S 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 h', E 4p ( Qf "CUD 4 1 rc AS bEKN APPROXIHATED bY A RECTANGLE TANGENT TO THK HALL IZK IS 20.250 20.250 25.000 TINE- "9 ~ 00 POOL bUSSLK DOHNCNb(ER SOURCE SDURCK SDDT RADIAL ANGULAR AXIAL DRAWING IHOKX INDKX RADIUS STRENGTH 'OCATION LOCATION LOCATICN AHGI.E ccowlgpt 1 I liono 6.070 181.Z5 7rooo 3.142 13.000 0.0 ~ t t 1.000 0.359 298.28 7.ono 2.356 l3oooo 05.ooo 3 3 liooo 0.359 Z98.2S 7.000 1.571 13.000 90.000 5 5 1.000 1.000 4.359 0.359 298 'b 29bitb 7onoo 0.785 13.ono 135.000 7.000 0.0 13.000 180.000 4 4 1.000 6.070 181.23 7 F 000 5.498 13.000 225.noo 7 7 l. 000 -6.070 181 '3 ~ 7.000 0.71Z 13.000 270.0no 8 8 1.000 do070 181 23 7.000 3.927 13.000 315. 000 <<>>>>>><<<<<<<<<<VELOCITIES AND ACCKLKRATIOHS AT GKOHKTRIC CENTERS OF 5(GIIENTS AT TINE>> 9.000 SECONDS>>>>>>>>>>>>>>>>>> f VELOCITY( T/SKC ) ACCELERATION(FT/SEC>>>>2) C/OL. V'O. Iij-l7, I)'j ~><-SOpu~- SEGHEHT Now Y Z RKSULTANT X Y Z RESULTANT O.tb 0.21 -0.4b 0.35 -O.20 1.08 0.19 1.21 0.05 12.90 -9.67 21.70 16.22 93.54 36.01 9d.SS 40.66 ( r.. I. ~ L pall r:s Ppdr c~'+ 0+15 0 F 00 0.28 -6.78 11.10 25.24 28.02 <<0.10 0.16 -0.07 0.20 0.47 7.21 21.35 22.90 0 ~ od 0.09 0.10 0.14 2.55 4.03 19.59 20.17 p ooP rCow~c.o~o>g g <<0.02 0.03 -0.11 " 0.12 0 '3 -1.30 lb.S7 lb.93 <<>>>>>>>>>><<>>>> VELOCITIES ANO ACCKLERATIONS NORHAL TO SKGHKHT AT TINE s 9.004 SECOHOS>>>>>>>>>>>>>>>>>> HORHAL VKLOCITY(FT/SEC) HORHAL ACCELERATION(FT/SEC>>>>2) SKGHKNT HO+ X Y Z RESULTANT X Y Z R E5ULTAHT -0.th -oo48 0.0 oo55 12.90 -21.70 0.0 25.25 -0.21 0.35 0.0 0.01 9.d7 16.22 0.0 lb.eS 0.15 -0 ~ 20 0~0 0.28 " -6.78 -11 ~ 18 0~0 13.07 0 ~ 10 0.16 0.0 oolb -0.47 7.21 . 0.0 S.08 0.06 -oo09 0 ' 0.10 -2.55 0.03 0.0 0.77 I 0.02 0 F 03 0 0 0+03 0.83 1.30 0.0 1.54 c <<>>>>>>>>>>>><<<< DRAGS AT TIHK s 9.000 SECONDS >>>>>>>>>>>>>>>>>> 'b SKGHENT NO+ k VKLOCITY DRAG (LBF) Y Z RKSULTANT X ACCELERATIDN DRAG'(LBF) Y Z RESULTANT TOTAL DRAG Y (LSF) Z RKSU(TANT 1 0.79 1.36 O.O 1.57 333.59 -561. 16 0.0 652.82 -334 38 -5d2.5Z 0.0 654.40 I 2 0,45 oott 0 '6 0.36 0.0 0+88 0.02 209+93 019.49 0.0 488.30 250 ~ 38 020.25 0.0 089. 1S 0~0 175.36 289.06 0.0 338.09 -175.58 -209.0Z 0.0 338.52 4 <<0.09 0.15 0.0 0.18 115.68 -186.32 0.0 219.31 115.77 -186.07 0.0 219.09 5 0.03 0.05 0.0 0+06 -d5.91 -100. 27 0.0 123.36 65.90 -1o4.32 0.0 123o01 4 0.00 0 00 0.0 oeol -21.03 -33.57 0.0 39.83 -Zli03 -33.58 0~0 39.80 TOTAL 1.58 2.68 0.0 3.11 -96).90 1593. SS 0.0 1861.72 -963.47 -159d.5d 0.0 1864.83 f<<8 H-FACTORS AT TIHE>> 9.000 SECONDS N<<8 1.000 1.000 1 F 000 1.000 1 F 000 l.ooo l.ono l.ooo l ~ g4 THl BUBBLE 5 bEEN APPROXIHATED BY A RECTAHGLK TAHGEHT TO THE HALL IZK IS MHCNSER 20.250 SOUR CK 20 ~ 250 25.000 SDURCK TINE<<10 ~ 00 SDOT RADIAL f A))GULAR AXIAL DRhHIHG INDEX INDEX RADIU5 STRENGTH LOCATION LOCATION LOCATION ANGLE 1 ~ Ii.)N e ~ 1.000 >>10 '69 197.dt 1.000 3.142 13.000 0.0 t 1.000 8.269 212 ~ 1d 7 F 000 R.356 13.000 45.000 3 1. 000 S.td9 RlZ.16 7.000 1.571 13.ono 90.000 4 1.000 8.269 212.76 F 000 0.785 13.000 135.0nn 5 5 1.000 bo269 tlt ~ 16 7.000 0.0 13. 000 100.00'0 4 4 1.000 10.769 197.62 7.000 5.498 13.000 tts.noo 1 7 1.000 loo769 191.62 7.000 4.712 13.000 270.000 4 8 i+000 10 'd9 191.dt 7.000 3.921 13.000 315.000 <<<<<<>><<<<<<>><<VELOCITIK5 AHD ACCELERATIOH5 AT GEOHKTRIC CENTERS OF 5EGHENTS AT TI)lK>> 10.000 SECONDS <<<<>>>>>><<>>>>>> SEGHEHT HDo VELOCITY(FT/5EC) Y Z RKSQ.TANT X ACCELERATIOH( FT/SEC<<>>2 ) Y Z RESULTANT cA L. /I/'0. >>) 77, 08 PX' 1 t Oosl 0.3b 0.87 -0.65 t,ll 0.43 t +33 0.86 lb.96 8.24 -lb.65 13.92 d0.94 lb.9Z d4,d1 24.89 0.27 -0.45 0.09 0.53 5.79 <<9.58 10.71 15.50 0.18 0 '9 <<0.04 0.34 -3.82 -6. 18 7.d7 10. 56 5 ~ 0.10 0.14 -Doll 0.22 2.17 -3.46 d.t6 7.48 4 >>oo03 0.05 Oo 13 0+ 14 0.71 l. 11 5,68 5.83 P ey 0 S O Vi>> C O ~ Z > /' <<<<<<<<<<<<<<>>a VELOCITIES AND ACCELKRATIONS NDRHAL TO SEGHENT AT TIHE ~ 10.000 SECDND5 <<<<<<>><<<<<<<<<< HDRHAL VELOCITY(FT/SEC) HORHAL ACCELERATIOH(FT/SEC>><<2) SKSHEHT HO+ Y Z R ESULTANT X Y Z RESULTAHT 1 -0.51 0.87 0.0 1.00 10.96 lb.d5 0.0 Rl.d3 2 0.38 -0.65 0.0 0 ~ 75 -8.th 13.92 0.0 16.17 -0.27 0.45 0.0 0.52 -5 ~ 19 9.50 0~0 11. 20 4 -0.18 0.29 0.0 0.34 -3.82 6.18 0.0 7.26 5 -0.10 -0 ~ 16 0.0 Oo19 2.17 3,4d 0.0 4.08 4 -Oo03 Oo05 0.0 0+06 -0.71 1.11 0.0 1.32 'swam<<<<e<<i 'ORAOS IT TIHK a 10.000 SKCOt05 <<<<<<<<<<<<<<<<a (~ '> ~ >a 'gg'ELOCITY ' DRAG (LBF) ACCELKRATION DRAG tLBF) TOTAL DRAG <LBF) .; P.) )KSH~,i~"".' Z RESULTANT X Y Z RESULTANT Y Z RES+TANT 4.53 o.o s.e4 283.42 482.33 0.0 559.43 -286.06 -486.86 0.0 564.68 -2 52 00 R93 -213.01 359.91 0.0 418.22 -214.49 -3dt.43 0.0 421.14 1.20 0.0 1+40 149.dl 247.80 0.0 289.49 -150.39 -249 F 01 0 ' 290.90 a !!ih .i '0.10 3, 0.31 0.50 -0.16 0.0 0.59 -'9S.12 159 '4 0.0 107.79 99 F 03 -56.32 -160.25 0.0 10$ .38 '.l~i$ ">]. I 0.0 0.19 56.22 89.43 0.0 105.63 -89o59 0.0 105.82 )'f'4',', ' oool 0 ~ OZ 0.0 O.OR -1S.27 28.80 0.0 34oll -lb.tS -Z4.82 0 ' 34.13 TOT+> '." -5.26 -8.93 0.0 10 37 -819.31 13dS.ol 0 ' 1594.67 -824.58 -1376.94 0.0 ld05.04 bib K FACTOR5 AT TIHK>> 10.000 SECONDS bob 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 f N ,l l AS bEEM APPROXIHATEO BY A RECTANGLE TAHGEHT TO THE HALL
- I":~'~(': l.":1e'T~ '! 'ECRCZTT DRAG (LBF) ACCELERATION DRAG.(LBF) TOTAL DRAG (LBF)
~ 13.000 0.0 t t 1.000 34.626 593.52 7oooo Z.356 13.000 45.000 3 loooo 34.82d 593.52 7.000 lo571 13.000 90.000 4 4 1.000 34.82d 593.52 7.000 0.785 13 ~ 000 135 F 000 5 5 1.000 34.8zd 593.52 7.000 0.0 13.000 180.000 4 d 1 F 000 1.335 135.03 7 F 000 5.49$ 13.000 LZ5,000 7 7 1.000 1 o335 135.03 7.000 4.112 13.000 210.ooo 8 b 1.000 1 o335 135.03 7.000 3.927 13. 000 315.000 <<<<<<<<xx<<x<<VELOCITIES AND ACCKLLRATIOHS AT GEOHKTRIC CKNTERS OF SEGHEHTS AT TItlK oo 11.000 SECONDS xxxxwxxxx 'KGHKNT Ho ~ VELOCITY(FT/SEC) Y Z RESULTANT X ACCELKRATIOH(F T/5ECxx 2 ) Y Z RESULTANT CAL. /}/o. /~~77. >> ux-boo+~ 1 t 4 1.00 -0.74 Oo52 0 ~ 34 1.41 1 ozl 0.84 0.54 12.40 dol7 5.06 4.d9 12,74 d 33 5.14 19.87 14.60 10.3d 32.71 o.4 ~ -lb.93 53 205.18 94.01 74.28 208.72 98.27 76.89 ;. g. Low 4 ~ 13 6.83 10.91 61.4d 6$ .6$ 5 4 ...-0 19 0.04 -0.30 0.10 4.52 4.46 4.54 4.46 3 ~ 90 lo27 -6.10 1.96 64,44 d3.22 6'4.85 d3.27 P oo~ oI< a~ como+S ) <<<<<<xxxx<<x VELOCITIES AHD ACCELKRATIOHS HORtlAL TO SEGHEHT AT TItlE <<11.000 SECOtlDS <<xxx>>xxxx HORklAL VELOCITY(FT/SEC) HORklAL ACCKLERATIOHlFT/SECxxz) SKOHEHT HOo X Y Z R ESULTAHT X Y . RESULTANT looo Oo74 1.41 1.21 0~0 1 90 1.42 19 '1 -32.71 0~0 38.27 0~0 14.80 24.53 0.0 28.65 0.52 0.64 0.0 oo98 loo3d ldo93 0~0 19.85 0.34 0.54 0.0 0.44 d o83 10,91 0~0 12.87 0.19 -0.30 0.0 0.3d -3 '0 dolo 0.0 7.24 o" 4 o ., Oood -0.10 0.0 Oolz lo27 1.94 0.0 2 '4
- i. slat Is to.zso zo.eso as.ooo TINE* 11.00 BUbBLK DOtbtCOt%KR SOURCE SOURCE SDDT RADIAL ANGULAR AXIAL DRANIHG INDEX INDEX RADIUS STRENGTH LOCATIOH LOCATION LOCATION ANGLE 1 o ~ ot<<t o loooo -1.335 135. 03 7.000 3.142
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'itobl 15.89 8.95 Ooo lbod7 10.48 -513 '0 362.48 645.77 0.0 909.55 523.51 861.66 0.0 1008.22 <<,} So45 0 0 434.41 0.0 740.69 -38S.13 643.36 0.0 751.37 I I .. o ':$ I'Ij,!o ~ ~ todh 4.29 0~0 5.03 -267. 80 <<431 ~ 82 0~0 513 F 23 Z7O,44 -442. 11 0.0 51$ ~ 24 EI'Ail,. 1 ~ 13 1.79 0.0 2 ~ lz -]76.69 -i82.17 0.0 332.92 -177.82 263.96 0.0 335.04 '1'Q' ~ 0,34 0.56 0.0 0.67 100.75 15'2 0.0 167.24 -101.11 158.3S 0.0 167.91 '.y.f 'l ~ o gO i i ~ ~ -0.04 0 ~ Od 0.0 0 ~ 01 32 '7 50 '9 0~0 40 ~ 45 <<32 F 81 -50.85 0.0 60 ~ 52 TOtj, -19.43 -31.54 O.O 31.OS -1474.39 -2408 '8 0~0 2824.Z1 -1493.62 2440.32 0.0 ZC61.32 ebb )l FACTORS AT TINK e 11.000 SECONDS bib 1 ~ 000 1.000 1.000 1.000 1.000 1.000 loooo 1.000 0 a'r 4= j t ~y lit Cf 't~ ~ ". 1 AS SKKH APPROXIIIATEO bY A RECTAHGLK TANGENT TO THE HAI.I POOL Tl SIZE IS Ro. 250 RO. R50 25. 000 TINE>> 12. 00 bUSSLE OOHHCO)%IKR SOURCE SOURCE SOOT RADIAL ANGULAR AXIAL DRAHIHG INDEX INDEX RADIUS STREHGTH 'OCATIOH LOCATION LOCATIOH ANGLE 1 ~ It)i( g loooo 9.389 180.51 1.000 3.14R 13.000 0.0 2 t 1 oooo 14.363 168.91 7.000 2.356 13.000 45.000 3 1.000 ld.3d3 145.91 7.000 1.571 13.000 90 F 000 1.000 ld.3d3 165.91 F 000 0.785 13.ono 135.000 5 5 loono ld.3d3 168 91 7.000 AD 13.000 180 F 000 4 4 i(000 9o389 150.51 7.000 5.495 13 F 000 ZZS(000 7 7 1,000 9.309 180.51 7.000 4.712 13.000 21o.ono 4 lo000 9.389 180.51 7.000 3.927 13.000 315.000 a>>aa>>aaa>> VELOCITIES AN) ACCKLKRATIONS AT GKOtlETRIC CKNTERS OF SEGtlENTS AT TIHE s 12.000 SECONDS <<>>a>>>>>>>>>>>> VELOCITYIFT/SKC) ACCKLERATIONIFT/SEC<<<<t) C SKGHEHT Hoo Y Z RKSULTAHT X Y Z RESULTANT CAL. 3~'n. /aJ vy, g$ -pp'$ 90~ ~ 1 0.49 -l,ld So lb 5.35 -9.31 15.90 4d o39 49.91 t 0.52 0.87 2o03 2.21 7.00 -11.86 1R.db 18.72 -0.34 -0.24 0.60 1,44 l.dl 4.92 -8.14 5.99 11.26 C. g. Lotto ow P-d s~ 4 0.39 1 23 1.31 -3.25 5.24 3(47 7.09 5 0 14 D.RR 1.14 1.17 1.55 R.95 R.31 4.17 4 0(04 0.07 lolo 1.10 0.40 0.95 l(52 RE 14 pooP dou)~(.((~ v(- ( ) >>>>>>>>>>>>>>>>>> VELOCITIES AHD ACCKLKRATIONS HORHAL TO SKGHKHT AT TIIIE>> 12.000 SECONDS>>>>>>>>>>>>>>>>>> HORHAL VELOCITYIFT/SEC) HOR)IAL ACCELERATIOHIFT/SEC>>>>2) 5KGHKNT HOo X Y Z RESULTANT X Y Z RE SULTAHT 1 3 t -0.49 0.52 0.3d <<1.14 -O.51 DodO 0.0 0.0 0 0 '.01 1.34 0 ~ 70 9.31 -7.00 4.92 -15.90 -11.56 -8.16 0.0 0.0 0.0 lb.43 13.77 9.53 4 0.24 0.39 0.0 0.44 3.25 5.26 0.0 6.15 5 0.14 0(RR 0~0 D.td -1.85 -R.95 0.0 3,4$ 4 Do04 0 ~ 07 0.0 0 F 05 -0.60 0.95 0.0 1.12 ( aa>>a>>aaaa DRAGS AT TIHK>> 12.00D SECOtE)S <<>>>>>>>>>>>>>>>>
- (<(((Ia AT TIKE ~ 11,000 SECOHDS <<xxxxxx<<<< I VELOCITY DRAG <LBF) ACCELERATIOH DRAG lLBF) TOTAL DRAG lLDF) I X Y Z RKSULTANT X Y Z R ESULTANT Y Z RESiA.TANT
NT gaol:. I X VELOCITY DRAG (LDF) Y Z RESULTANT X ACCELERATIOH DRAG Y Z (LSF) RESULTANT TOTAL DRAG ILBF) Z RES(LTAHT 9.54 240.12 -411.27 0.0 476,54 -R45.60 419.47 0.0 454.OS 5.34 -181. 11 -306.69 0.0 356.18 3dl.52 ";;:, 3... o'.33 I -2.19 0.0 2.5d 127.31 Rll.ll 0.0 R46.53 183 o 54 -125.64 311.25 213.30 0.0 0.0 249.09 1.05 53,95 136.09 0.0 159.9(2 54.54 -137.01 0.0 140.99 1 0.34 41.8Z -7d.19 0.0 89 ~ 94 -45.00 7d,4$ 0.0 90.30 0(04 15(54 <<24(54 0.0 R9 F 05 lb.56 -24.57 0~0 29.05 'il I. <<9.1t ld.tl ooo lb.90 694(41 lld5o90 0~0 1355.1d. 706.1S -1152.11 0.0 1'377.06 458 N FACTORS AT TINK>> 12 ~ 000 SECONDS 515 (. (-.tl,o . , 1.000 1.000 1.000 1.000 loooo 1.000 1.000 1.000 i ( o * ((o g) ~r <<H1 "1a CK-l P'f I, 'I tl ( II bKKH APPROXIHATED bY A RECTANGLE TANGENT TO THK HALL IZK I5 20 R50. 20 250 R5.000 TIKE<< 13 ~ 00 bUbbLK DD)NCOtItKR SON)CK SOURCE SDOT RADIAL ANGINA AR AXIAL D RAKING INDEX IHDKX RADIUS STRENGTH 'OCATION LOCATION LOCATION ANGLE 1 1 i ~ MQ>>v i 1+000 -d.243 173.27 F 000 3 ~ 142 13 F 000 0.0 t t 1.000 5 714 5.714 325.11 325. 11 7.000 7.000 2.35d 1.571
- ~ '...
<<>>>><<>>>>>>>><<VELOCITIES AHD ACCKLKRATIDHS AT GEOHKTRIC CEHTER5 OF 5EGHEHT5 AT TIHE s 13.000 SECOND5>>>>>>>>>>>>>>>>>> VELOCITY(FT/SKC) ACCELERATIDHtFT/SEC>>>>2) Y Z RESULTANT X Y RES)A.TANT 1 0.32 0.54 1 5d l.db -13.44 -22.53 104 ~ 00 107.24 2 <<0.24 0.17 0.41 -0 28 0.42 0 19 O.d3 0.38 10.06 7.05 16.85 11.41 41,6d 30.10 46.05 33.02 C C ~ 0 ~ L go.d r)~ t'urIrg+r5 -" 0.04 -0.11 ~ -0.18 0.10 0 '4 4.d5 -t.d5 -7.49 25.96 '9 27.42 5 -0.10 0 F 06 0.13 4.19 24 24.do 6 'oot 0+03 0.05 0.06 0.86 l.'35 23+33 23.39 pod ) d 0>g~g p~~ i g ) r <<>>>><<>>>>>>>><<VELOCITIES AtO ACCKLKRATIDH5 HDRHAL TO SKGHENT AT TIHK <<13.000 SECONDS>>>>>><<<<<<<<<<>> HORHAL VKLOCITYtFT/SKC) NOR)tAL ACCELERATIONl T/SEC>>>>2) f SKNIKHT lC) ~ X Y Z R ESULTANT X Y Z RESULTANT 1 -0.32 -0.54 0.0 oo63 13.44 22.53 0.0 Zd.Z3 Oq 2 0,24 oo41 0.0 0.47 10 ~ 06 -14.85 0~0 19.dt O.17 -0 F 28 0~0 0+33 7.05 11.61 0+0 13 ~ 59 <<0.11 0.18 0.0 0.21 4.45 7.49 0.0 8 ~ 81 5 0.04 0 ~ 10 0~0 O.lt 2.4$ -0 ~ 86 4 '9 0.0 4+96 1.60 0 6 ~0 ~ ot -0 ~ 03 0.0 0,04 1.35 0.0 'I 'ii r i', '>>>><<q<<<<<<j ~'.,HW ~ 'i >>i.":A bttltKHf'+'I,"J.I = X AT TINK ~ Y 13.OOO SECONDS <<>>>>>>>>>>>><<<< VELOCITY DRAO tLbF) Z RESULTANT X ACCKLKRATIOH DRAO Y Z tLbF) RESULTANT TOTAL DRAG Y tLbF) Z RKSUt)TANT I t.07 347.45 582.50 0.0 d78.R5 348.49 -584otb 0.0 d80.3t '> .'3~ " 'I,".'; h <<<<io.lt ~0 ~ R9 0.47 0.20 0~0 ooo 1.15 0.5$ 0.23 260.08 -182.41 <<1R0.33 435.d7 300 193.55 '9 0~0 0.0 0.0 507.40 351.35 227.91 -260.67 letid9 -120.45 436.67 300.76 -193.75 0.0 0+0 0~0 508.55 351.90 228. 14 'l 0 ~ 07 dba57 108.31 0.0 128 ~ 19 -60,dl 108.37 0.0 12S.2d i ~ 0 ~ ol -22.29 -34.87 0~0 41 ~ 39 22.30 -34.8S 0.0 41 40 TDTa4->I.';I'i -t.ob ~ ~ -3.52 io.o 4.o9 -loo1.13 <<ld55.19 0~0 1934 '8 -1003.21 ld58.71 0.0 1938 57 888 K FACTORS AT TIHK a 13.000 SKCONDS O<<8 I 1.000 1.000 1.000 liooo 1.000 1.000 1+000 1+000 L I~ LIP IWlk 4 I. t./ f I 4} Cf ~, t'[ 'I S / Tg Ck I 4e 4 V, ~ t.J ~r P, bKKN APPROXIHATED BY A RECTAHGLK TAHGENT TO THE HAL IZE IS ROoR50 tO ~ 250 R5 000 TINE<< 14.00 bUbbLK DD)NCD)b(ER 50URCK SOURCE SOOT RADIAL ANGULAR AXI4L DRAHIHG INDEX INDEX RADIUS STRENGTH LOCATION LOCATION LOCATION ANGLE 1 og>oo > 1 ~ 000 10.dZO 273.tO 7.000 3.142 13.000 0.0 2 t 1 ~ 000 7.488 474.26 7>000 2.354 13.000 45.000 1.000 7,488 47d.26 7>000 1.571 13.000 '90.000 4 1.000 '7 488 47d.26 7 F 000 0.785 13.000 135.000 5 5 1 ~ 000 7.4SS 47d.26 7.000 0.0 13.000 180>000 4 4 1.000 10.dZO 273.24 7.000 5.498 . 13 ~ 000 225.000 7 7 1.000 10.424 -273.24 7.000 4.712 13 ~ 000 270.000 8 8 1.000 10.624 273.24 7.000 3o927 13 F 000 315.000 <<<<<<>><<<<<<<<<<VKLDCITIKS A)Q ACCKLKRATIDN5 AT GEOHETRIC CKNTER5 OF SEGHENT5 AT TIHE>> 14.000 SECONDS>>>>>>>>>>>>>>>>>> VKLOCITY(FT/5EC) ACCELERATION(FT/SEC<<>>R) SKQHKHT Hbo Y Z RESN.TANT X Y Z RESULTANT CAL. >L/o. Iol77 08 >1/-doO+2 ~ 1 0,48 0.83 1,83 R.07 -20.18 33.90 150.71 155. 79 0.34 >>0.42 0.30 0.7S 15. 12 25.35 59,10 66.06 R 3 0.25 0.17 0.42 0.27 0.01 0,14 0,49 0.35 10 ~ 60 6.99 >>17>47 11.26 42 '2 35.88 46.73 C C 0 ~ LO>>.d oo, 'urlqs4og 38.25 5 0.10 0.15 0.19 0.26 3.99 4.30 33.10 33.93 4 0>03 Oo05 -0>RR O.R3 l>30 2.03 31.97 32.06 pooD J>~~co~.~z ) <<<<>>a<<<<<<>><<VELOCITIES Ne ACCELKRATIOHS NORHAL TO SKOHKHT AT TIHK>> 14.000 SECOHD5 <<>>>>>>>>>>>>>>a HORHAL VELOCITY(FT/5EC) ACCELKRATION(FT/5EC>>>>2) Y Z RESULTANT Y Z RESULTAHT 1 t 0>48 0,36 0.83 O.dt 'R0.18
- 13. 000 13.000 45.000 3 1,000 90oooo 1.000 5.714 325.11 7+000 0 ~ 785 13.000 135.000 5 5 l+000 5 '14 325,11 7.000 0.0 13.000 leO.O0O 4 4 1.000 do243 173.27 F 000 5.498 13.000 Z25 F 000 7 7 1.000 d.R43 173.27 7.000 4. 712 13.000 270.000 8 8 lo000 de243 173.27 7 F 000 3.927 13.000 315 F 000
4 -0>17 0.27 -6.99 ll.td 0.0 13 F 26 5 0>10 0.15 3,99 d.30 '.0 7.46 ;f 4,, ...", )0>03 0 ~ 05 1.30 R.03 0>0 2.41 '." .!,,1 '()g J'T TIHK e 14.000 SECDND5 a>>>>>>>>>>>>>>a l ACCELERATION DRAG (LBF) TOTAL DRAG (LBF) ( X Y Z RESULTANT Y Z RESULTAHT -521.90 -87d.dt 0.0 1020.22 -524.29 -880.73 0.0 1024.97 -390.86 -d55.47 0.0 763.ld -392.20 -d57.75 0.0 7d5.81 274>19 451.72 0.0 528.42 R74.85 452.81 0.0 529.d9 -180.88 291.17 0.0 342.77 -181.16 -291.6Z 0.0 343.31 <-'.'4" .i" 0 '9 0.14 0~0 0 '7 103.06 162.94 0~0 192.80 103.15 -163.08 0.0 192.97 D ~ 1> +0 ~ 01 -0 ~ Ol 0.0 0.02 -33>51 -52.46 0 ' dt>25 33.52 52,4S 0.0 dt>Z7 TOTAL ~ .' 74 8.0t 0.0 t.3t 1504.41 2490.38 0.0 2909.d3 -1509.17 -2498.47 0.0 2919.01 ~, . Slb 4 H FACTORS AT TINK>> 14.000 5ECDHDS SNS > ~ 3 > o ~ ~ ~~ ~ 1o000 1 ~000 1~000 1 ~000 1~000 1.000 1.000 1.000 >> o>y ~ ~ 0 + t>> +1(ti . o tg, Q+ g(f " 'ykeg < j ~ I i~1 s bLEH APPRDXIHATKD bY A RECTAHGLK TANGENT TO THK HALt E IS 20.250 20.250 25.000 TIHEa 15.00 bUbbLE DDtitCOtitER SOURCE SOURCE SDDT RADIAL ANGULAR AXIAL DRAHIHQ IHOKX I)OKX RADIUS STRENGTH LOCAT IOH LOCATION LOCATION ANGLE . 1 I s ~ ')He 1.000 -1.613 103o24 7.000 3.142 13.000 0.0 2 R 1+000 4 744 123.d5 7 F 000 2.356 13.000 45.000 3 1.000 4 744 1Z3o65 7 F 000 1.571 13.000 90 F 000 4 4 1 F 000 4,744 123.45 F 000 0.785 13.000 135+000 5 5 1.000 4 '44 123.d5 7.000 0.0 13.000 180.000 4 4 1.000 <<l.d13 103o24 7 F 000 5o498 13.000 225.000 7 7 1.000 1.413 103.24 7a000 4.71R 13.000 270o000 4 8 1 ~ 000 Ie413 103.24 7 F 000 3.927 13.000 315.000 a>>a<<a>><<aa VELOCITIES AtO ACCKLERATIDNS AT BEDHETRIC CENTKRS OF SEG)IEHTS AT TIHE ~ 15.000 SECDHOS a>>a>>>>>>hw>> VELOCITYtFT/SEC) ACCELERATIDNtFT/SEC>>>>R) SEGHKNT HO ~ Y Z RESISTANT X Y Z RESULTAHT 1 0.17 0.29 i+59 l.d3 4.07 10.30 3d.40 lb.31 2 Ool3 '9 0.21 0.70 0.54 0 '4 0.56 4.5d 7.d9 -5.30 1R.14 15.08 C C ~ 0 L o~d o~ P~he~+~3 I I I 3 0 Ool5 F 20 7.46 9 ~ 70 I 4 0.04 0.10 0 48 0.49 Roll -3.41 5.74 7.01 I 5 0 '3 0.05 0.45 0.46 -l. RO 1.91 4.95 5.44 'I 4 Oo01 0 F 02 0.44 0.45 Oo39 0.62 4.62 4.dS j>ooP dpivo,co~op g ) aaaaaaaaa VELOCITIES AtO ACCKLKRATIOH5 NORHAL TO 5KGHENT AT TINE a 15.000 SECD)OS a>>awaa>>aa HORHAL VELOCITYtFT/SEC) HORHAL ACCELERATION(FT/SKC<<<<2) SKQHKHT NO+ X Y Z RESULTANT X Y Z RESULTAtlT 0 ~ 17 <<Oo29 8.0 0.33 <<4 07 <<10.30 0.8 11.9d <<Oo13 O.Rl 0.0 0.25 4.56 7.d9 0.0 8.94 ) 0 09 0.15 0.0 0.17 3o20 5.30 0.0 6,19 <<Oo06 Ool0 0.0 Soll R.ll 3.41 0 ' 4.01 5 0.03 0 ~ 05 0.0 0 ~ Od 1.20 1 91 ~ 0'.0 R.Z6 4 OoOI Oo02 0+0 0 F 02 0.39 <<O.dR 0.0 0.73 ,~ '<<attai4~ DNA'T TIHK s lb.000 SECO)OS <<aaa>>aaa>> i 4't <> t"."i- i '-. t, (. gj,l '! > ~t~ ~ ji ~ ~ VELOCITY DRAB tLbF) ACCELKRATIOH DRAG tLBF) TOTAL DRAG tLSF) t X Y Z RESULTANT Y Z RESUPANT 0.50 0.0 0.58 156 99 2d6.37 0.0 309 F 19 -157.29 -Rd6.8d 0~0 309 77 0.28 0 0 0.33 117. 89 198.85 0.0 Z31.17 -118.06 -199.13 0.0 231.49 0 13 0 0 0.16 -82.80 13d.94 0.0 160 ~ 03 -SR.OS 137 08 0~0 ld0.19 I l 0.06 Oa0 0 07 54.42 88.28 0.0 103 ~ Sl 54.65 -88.33 0.0 103.87 0.02 0.0 0.02 -31.11 -49.41 0.0 58.39 ,-31.12 -49.43 0.0 58.41 0.00 0,0 0 F 00 10.11 15.91 0.0 1S. 85 10 ~ 11 -15.91 0.0 18 ~ 86 I "p)A)'";;";, -)~.40 -0.98 0.0 1.15 -453.52 -755.76 0 ' 881.44 454.11 754.74 0.0 8SZ.58 r; s BIB'.g '" '.000 FACTORS; AT TIHE a 1.000 15,000 SECONDS 8%8 1.000 1.000 1.000 1.000 1.000 1.000 gC gS tg / V '~~<< isa.vsalltb At~0 ALCELtRA)IONS HQRNAL TO SKGNEHT AT TIHF D SKCO)SS <<<<<<<<<<<<<<<<>> HORNAL VELOCITYlFT/SKC) HORllAL ACl. lFT/SEC<<<<Z) ~ X Y R RESULTANT X o Z RESLATANT 8o17 bott 0.0 0.33 4.07 el0.30 0~0 ll.td Oo13 O.tl 0~0 0.25 -4.56 l.d9 0.0 So94 0 ~ 69 0 ~ 15 0.0 0. 11 3.20 5.30 0.0 6.19 0 ~ 06 0.05 -0.10 0.05 0.0 0.0 0.11 0.06 t.ll 1.20 3.41 1.91 0.0 0.0 4.01 2.26 0o01 -O.OR Oo0 0 F 02 Do59 0.6Z 0.0 0 ~ '23 a>>a>>>>>>aaa DRAQS AT TINK a 15.060 5KCOHOS>>>>>>>><<>>>>a>> ~ VELOCITY BRAS lLBF) ACCEl.ERATION DRAG lLBF) TOTAL DRAG lLBF) SKQNKNT )0>>' X Y X RKSULTANT X Y RESULTANT Y R RESUPANT 1 0.30 0.50 0.0 0.55 -156.99 Rdd.37 0.0 309.19 -157.Z9 -Zdd.Bd 0.0 309.77 Z Doll 0.28 Oi0 0.33 117.89 195.85 0.0 Z31.17 -118.66 199.13 0 0 231.49 3 0.65 -0. 13 0.0 0.16 82 '0 136.94 0.0 0.0 ldO 05 -82.65 137.05 0.0 ld6.19 4 0 05 D.od 0.0 0.07 54.62 88.25 103 81 >>54.65 68.33 O.o 165.82 5 Oi01 -D.ot 0.0 0.02 51 ill 49.41 0.0 56.39 -31.1Z -49.45 D.O 55.41 4 Oi00 0.00 0~0 0 F 00 10,11 >>15.91 0.0 lb.85 10.11 15.91 O.D 1S ~ 86 O,d0 1 98 OoO lol5 453 i52 155.7d 0.0 651.44 -454.11 256.74 0.0 ee2.55 bbb N-FACTORS AT TIHE a 15,110 5KCOHDS SOB liOOD 1.000 1.000 1.000 1.060 lo000 io000 1.000 StbHKNT NOo X D.45 HORNLL Y, 0.71 VKLOCITYlFT/SKC) R 0~0 RESULTANT
- 15. 1Z 33 '0 25.35 0~0 0.0 39.45 t9.51 0>25 O.OR 10>d0 17 '7 0.0 R0.43 (
-21.19 0.0 0*0 33.92 25 ~ 57 ~ g 1 0.67 13 ~ 00 11. 51 t 0 ~ 54 -0.24 0.55 -0,40 0~0 0.0 0.46 9,12 15.02 -9.65 . 0.0 0.0 11.40 -6.02 ~: . " 4 ~ '.14 0.26 Do14 0.0 AD 0.30 Dill 3.43 5.4R 0.0 6.41 2 ~ 01 ~ 0,05 1.11 1.14 0 0 F 05 Oo0 ~ .' 4 ",; l l'~0.03 TIHE s ld.001 SKCO)OS a>>>>a>>>>a>>a TOTAL DRAG tLBF) ACCKLKRATIDN DRAG lLBF) Y R RKSUltTANT \ VELOCITY DRAG lLBF) R RESULTANT "', Y ~ y X dt0lOHT Ntw "i ', X Y Z RESlLTANT 8'27. 12 451. 09 -757inb 0 ~0 551 ~ tb . 3.59 0~0 4.ld ~44bott 33d 18 155.49 563.47 Oi0 0.0 456.14 351 '6 R3d,5b 565.47 -569.30 0.0 0.0 655.4d 455.44 0 ~0 Ro32 0.0 454.53 295. 15 ' +Iolb R.OD 255. Sl 36S.35 -250.71 0.0 s', '. o 'pit ';3 j $ ') 0.51 0.95 0.0 1.11 250.32 0.0 294.21 1'55. 80 0.0 ld5.91 ~ 5s,% ':-'0.25 ~-'.-O.OS 0.40 0.13 0.0 0,0 0.4'2 0.15 155. 56 -88.64 ~140.66
- 0. 69 17.3d 29.14
-88.12 25 83 140. ZO -45. 11 0.0 55o54 0.02 25.52 o ' ! 001 -0.01 0~0 -1295.17 -2147.6S 6.0 Z569 51 R140. 80 0.0 2501.59 1295.98 TOTAL . 4 lt 7.05 0.0 ~ 8. 23 << 16 F 000 SKCONDS . 1.000 ~ Bb N-FACTORS AT TINE 1.000 1.000 1,000 1.006 1.000 1,060 1.600 ~ pg l>o JP IV r. 'bI 44 4 fk N 4q 1 i l~ HAS BKEH APPROXIHATED bY A RECTANGLE TAHGEHT TO THE V E POOL SIZE IS RO. 250 RO. 250 Z5. 000 TIHE* 17. n uwglg SOURCK SOURCE SOOT AHGULAR AXIAL DRAHIHG INDEX Ite EXid~>'bat I'ONHCO)SIKR RADIUS STRENGTH RADIAL'OCATION LOCATION LOCATION- AHGLK 1 .1 I I 000 156.91 7.000 3 ~ 142 13.000 0.0 t t 1.000 -8.547'.323 287.56 7o000 2.356 13o000 45.000 1.000 3 o32'3 287.56 7.000 1.571 13.000 '90.000 l: 5 4 5 1.000 1.000 3.323 3.323 . 287.56 ZS7o56 7.000 7.000 0.785 0.0 13.000 13.000 135 F 000 180 F 000 4,: g, ~ 6 7 8 lo000 1 F 000 1.000 8.547 8.547 8.547 156.91 156.91 -156.91 7+000 7 F 000 7.000 5.498 4.712 3.927
- 45. 10 0.0 0.0 145.17 55.52
<<aaaaaaaa VELOCITIES AND ACCELERATIONS AT GKO)IETRIC CENTERS OF SEGHENTS AT TItlE i 17.000 SECONDS <<aa>>aa>>>>a VELOCITY(FT/SEC) ACCELERATION(FT/SEC<<<<2) SKGHEHT HO ~ Y Z RESULTANT X Y R RESULTANT 1 Oo31 Oo54 0.49 0.80 11.98 20.09 91.68 94.62 t 0.24 0.40 0.25 0.53 -8.97 15 F 03 36.48 40.4d -0.17 Ootb -0.41 0.53 -d.R9 10.36 Zd.23 28.90 0.11 Oolb 0 ~ 48 Oo53 4.15 -d.db 22+56 23.89 ~ 5 6 Oobd 0.02 0.10 0.03 -0.52 Oo53 0.53 0.53 2.36 <<0.77 -3.74 1.ZO Z0.90 20.22 21.3d 20.27 C C. 0. Lnnd /'o d n S +CcP P~ ~ ) ~0 ~8~80~ u I- S ) <<aaaaaaaa VELOCITIES AHD ACCELERATIOHS HORHAL TO SEGHEHT AT TItlE a 17.000 SKCONOS a>>a>>a>>a>>a HORttAL VELOCITYlFT/SKC) NORllAL ACCELERATIONlFT/SEC>>>>2) ,4 SKGHENT HO ~ X Y Z RKSULTANT X Y R RESUI.TANT ~ N 1 Oo31 0.54 0.0 O,d3 11.98 20.09 0~0 23o39 hg t Oot4 0 40 0.0 0.47 -8.97 15.03 0 ' 17.50 I 3 0.17 0.28 0,0 0.3R d.t9 -10.36 0.0 Itilk 4 0.11 -0.06 0.18 -0 0~0 0.0 0.21 -4.15 6.db 0.0 7 '6 5 10 0.1R 2,3d 3.74: 0.0 4.4 2 6 O.OR 0.03 0.0 0 F 04 0 '7 . -1.RO 0.0 i+43 <<aaaaaaaa DRAGS AT TIHE a 17.000 SECOHDS aaaaaaaaa VELOCITY DRAG tLBF) ACCELERATION DRAG (LBF) TOTAL DRAG [LBF) SKGHKNT tQc ' Y t RKSULTANT X Y Z ~ RESULTANT Y R RESUl TANT 2, 1 3 loOk 057 0 28 -O.lt 1.78 -0 ~ '99 0.47 0 20 0.0 0.0 0.0 0~0 t.05 1.14 0.55 0 '3 309.75 R31.90 16Z.d5 107.30 -519.61 388od0 267.83 -172 '3 0.0 0.0 0.0 0.0 d04.93 452.54 313.35 203 '6 '10.77 -232.47 162.93 -107.42 -521.39 -309.59 Zdb.30 -172o83 0~0 0.0 0 ' 0~0 606.98 453.6S 313.90 203+49 5 6 '.00-0.04 0 06 0 ~ 01 0.0 0 ' 0 07 F 0.01 61.14 -19.88 -96.61 31.10 0.0 0+0 114.33 36.91 -61.18 -19.88 -96,d7 -31. 11 0.0 0.0 114.40 3d,92 TOTAL -2.03 -3.49 0.0 4.04 -892.63 -1476.39 0.0 1725.33 -894.66 -1479.88 0.0 1729.37 SOS H-FACTORS AT Tltlk + 17 ~ 000 SCCCN"S>>tw 1.000 1.000 1 F 000 1.000 1.000 1 F 000 1.000 1.000 A ag l,l wl 0 I V II li-A A" \'L /i I VJS-SO(WCK1(190 E6ION=d40K >> TIHE%2 >> DRIVES<<l / 5 PEN%.3))H>>IW<<CARSON>>PAPER<<ll>>GRID>>TIHK%30HIN /<<RUUTE PRINT CH /<<FICHE TITLEls 12177-PX d005t-2 COFSI SO(WCK TITLEts>> 50(NCE>> V.J.SHAH RN'<<FICHK ORIG5*3 CHOC/3G'<<FICHE /<<FICHK COPIES%3 /<<fICHK ORIGTOsl RECORD RFTKNTION CENTER- 1 ORIG /<<FICHE ORIGTOst V.J.5HAH>> CHOC/36 /<<FICHE COPIESTO%3 V.J.SHAH CHOC/36 //CALCOt0>> KXEC CS)PX >> LI)00(EH+CTLCDS >>HOOEL<<SOURCE // Tlt(E.X<<(2>>0) >>RE6ION.X=d50K e //X.fTOBF001 DD SYSOUT>(R>>RF f1) //X.CO(PRINT DD OU)R(Y DISPEL(NEH DELETE) //X.SYSPRINT OD DURITY ~ OISP%(HEH>>DELETE) //X.FTOdF001 OD SYSOUT=(R>>Rff1) //X.FT35F001 OD UNIT<<DISt( DSN 6ECO031.5T307.T0507 // DISP=SHR ~ //X.PLOTTAPE DD SYSOUTiP //X.SYSIN 00 << fIXEO IBUF e J ~ I / DItlEHSIOH IBUF(2000) >>PIl5) TITLE PRES5URE TINE HISTORY RUN 003 05-07 5KC. SYSTEH )0>>OINTa40000 INITIAL INCON SWITCHED.0 A<<144./(1,94%2.82 ) NOSORT If(SWITCH.KQ.t. ) CALL FINISH 101 fORI(AT( 2K13.5) T<<0.00 Pt(AX%0. . P)IIN%0. t00 RKADl35>>101) TIHI>>PINI P-"PIHI TESTRT CALL FGLOAD(C04T>>T>>P) 102 READ(35>>101>>KN0=104) T>>P 201 If(Pt(AX.LK.P) PHAX=P IF(P)IIN.GE.P) PHIN=P T>T-TINI IF(T.LK.TEST) 60 TO 102 TESTsT CALL F6LOAD(CO4T>>T>>P) 300 COHTINUK 60 TO 102 104 REWIND 35 T F 18 T+. 001 TftaTtl.O CALL fGLOAD(C04T>>Tf1>>0.0) CALL FGLOAD(CO4T>> Tf2>>0 ~ 0) PABS=PHAX IF( ABS(P)IIN) .GT.PASS)PAb$ %ABS(PHIN) I d e 1 0 d )T e P WR T E ( WRITE( d >> 108)Pt(AX>>PNIN>>PABS 10d FORt(AT( 1Hl e . ~ . FINAL TINE>' F8 ~ 4 ~ FINAL PRESSURE> >>FB 4) 108 fOR)IATl 1X t(AX PRESS(A)E%>> ~ F8 4>> e t(IN PRESSURE>>FB ~ 4 ~ ~ ~ flAX ABS PRESS(%K%'8.4>> 'AX LOAD(IBF)='9.2) ~ ~ 11~ IWE Oo FL 4 CO4T P4TCOs'AFGKN(CO4Ts TINK) SOOT*AssP4TCO 5$ *INTGRLl0.sSOOT) NKTHOO RHS TIHER FINTINi3.00sOELTs.001 sPRDELs:0.1sOUTDELs:0.001 fINISH TIHE*T RANGK 55sSDOTsP4TCO PRINT SSsSOOTsP4TCO TERHINAL HOSOR7 CALL OUTPUT W N Ifl5HITCH.KQ.K.)GO TO %99 IFlSHITCH.KQ.1. )60 TO 99b lfl SNITCH.KQ.O. )60 TO %97 60 TO 1000 999 CALL PLOT(0 ~ s0 ~ s99'9) 60 TO 1000 997 CALL PLOTSlIbUF st000) SNITCH*1. 99b CONTIWE 1000 CONTINUE PAGE XYPLOTsHEIGHTs4. sNIOTNsb. LASEL CO RLN 003 05-07 SEC. OUTPUT TINK sSS OUTPUT TIHEsSOOT OUTPUT TIHE sP4TCO Kte s~( Cr $1 't !.cQ 'j, />>J'ION>>700H) TIHE>>l />>R NT CH //>>. JK VJS-SSLDAD3:198 />>FICHE TITLEls'I2177.28-FK)(C)-PX-60052-t)005)CO LOAD ON D.C. ~ /FICHE TITLEtg)3/t4/87)HE*229)V00)LOO)V.J.SHAH/CHOC 3$ ) />>FICHK ORIG5=3 />>FICHE COPI ES*3 />>FICHK ORIGTO=RKCORD RKTKNTION CENTKR -1 ORG />>FICHE ORIGTO>>t V.J,SHAH CHOC/3G />>FICHK COPIESTO>>3 V+ J.SHAH)CHOC/3G //HOI EXEC PGH=SSLOAD)REGION=SOOH) TINE):5 //STEPLIS DD DSN<HE229 VOOLOO,LOAD)OISP SHR //FTOdF001 DD SZSOUTN(R)Rf f1))DCb=PRINT1 //FT10F001 DD>> C.O. LOAD N DNKOHERS PX-60052-t) RW 03)05-07 SKC. 14.167 45.5 176. Eol. 1 1.45t t.t 0.0 1.94 18 0 34.5 190 0 lb.0 34.5 tolo t.o />> //FT70F001 DD >> 8 1.0 34.5 lb.0 3 1.0 39.5 9.0 1.0 39.5 lb.0 1.0 39.5 27.0 1.0 34.5 9.0 1.0 34.5 F7.0 1~0 t9.5 4.5 1.0 t9.5 22.5 1 0 29.5 40.5 />> //FTbof ool DD a ZKS 5 39.5 34.5 t9.5 t4.5 19.5 0.0 0.0 1.0 4.5 4.5 9.0 9.0 lb.0 lb.0 lb.0 0000010101110011100000101010011101010100000000000000100000000000000000 ~ 'I1L,,3 0000000100000000111100000011110000000000000000000000000000000000000000 -'" '1".ii'> tt 1 189. I,!fd.. j ,N>> +'l0(!.F ;dO tod 00 F j)ji>>/II ;i48 fgO 206.00 cod.OO <OO 7$ .00 7$ .00 75.00 75.00 'i'! !,'j r~' -75.00 75.00 75.00 '.1o 75.00 fQ(j! 75.00 75.00 ,Nkllt(l .o:.l "'. 3.5.1>t'-'g ~ -75.00 tod.oo S.o,t! 0'. ~ As.oo t06.00
- 13. 000 13.000 13.000 225.000 Z70.000 315. 000
0 V ~ l, h /Z177. -/YPQ) PX- 6 o/60-0 Am~mw~i i~~ur J )s>>~c gee,r.~) 000 0DD0 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 00 OOD ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0 0 ODD ~ ~ 0000000ODOOOOOO 00 00 00 00 0O 00 0 ~ ~ ~ ~ 00 00 0000 0 00 00 000 00 0 00 00 0 ~ ~ ~ ~ 00000 D00 0 0 0 ~ ~ ~ ~ % IO % OOD 0 0 0N D w IA ih Ih In Ih Ih In lh lh Ih Ih lh Ih lh lh Ih ln In IA 'ICI 'In ICI '0 % 'CI '0 'C % 'III '0 Dt I PI I I I II I tI II PC I II Ir'I I II 000000000 ~ ~ ~ ln In In In 0 0 0 DDDPrPrtrPrlrWDDDDDCrP ln In ~ ~ ~ D ~ In ln lh Irlln NNN NN N N I I I I I PP ~ NNNNNNNNN0NN 00 ~ ~ ~ I N N NN NNN I I I I I I NNNNN I I I I 0 00 000000 00 00~ 00 00 00 00 00 0000 D0 0 0000 DOO OOOO 00 O ~ 00 0O 00 OOOOOO ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 00O ~ 0 00 0 0 0 0 0 0 0 0 0 0 0 0 0 0 D 0 0 0 O'0 O 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0O r 0 0~ 04 0+000 0 0 0 0000~ 0 0 00 w <<. r. << ICI ltl ltI In ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ Ie Ih ln In In Ih tC tC PC lrl Yl H Irl ltl Itl Yl lrl ltl e PI PI ln ln Irl ltl tC HtttCtf tltC IPI te Ih lh In In MI In In Ih lh In In Ih ln In In In lh ~ Ptg ~ ARM ~ ~ >44 et%%4t% gB ~ ~ ~ 4 PC tC ~ I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I 0 0 O.ODO ~ ~ 000000 00r 0000000000 000000000 000000 ~ ~ ~ ~ CC ~ ~ ~ ~ ~ ~ ~ Pl tC tC Pl tC tC tC ~ ~ ~ ~ ~ ~ tCtCPCtttCtf tCHtCt4 ~ ~ ~ ~ tC tC tl tC tC tC tC tC tC tC tC t4 tC tC ~ ~ PC ~ ~ ~ ~ ~ ~ 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 00 0 Oe"i&++exy'Cr~b~&ae <<+Q %ussrr <<rr .t ~Pl~Cna'v e. lrl Yl Itl Inlnln lnln pl pl pl s a pl ltl lnnlnln pl lnlnln s lnln s ln In pl pl s plln pl pl plea pl PI In ltl N.r ICLQ'~$ ~A+Qg o w r ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ +C r ~'T 'I r V +e 4 a '1 +I y -a, fZ/77.28 Pic) PX- dotdg-u //YPD7 Llsi tHG /Glar.~g OOCi oa 000 0 O o0 00 Oao 0 O oa 0 0 0 0 OOOO Ci O 0 0 OOOO ao oa 0 CI 0 0 0 0 0 0 0 0 Oooo oa 0 0 DODO 0 0 0 0 0 0 0 ~ ~ ~ ~ \ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ lh IJI IJI Ih lh IA & % m lh lh lh lh lh lh lh Irl IA IA w w w ~ ~ ~ '0 r 0 0 0D00 % I I I I I I N NN NN N W N N W I I I I I I I I I r I ooo CI 'CI W lO ~ I r 0 0 0 or r I r 0N 00 DO0 NMN N N N NN Daa 00 00 Ci0 0 0 0 DODD 0 D ao Doao ODD OOOO 0 0~ o Oa O O 0 D 0 o 0 oooo 0 0 OOOO 00 ao iri nn Ie n IJI ~ I I ~ ~ ~ I I I I ~ ~ O kkk k Ill Ih IA IA Ih IA Ih lh IA IA nk kkkk ~ I I I I ~ ~ ~ ~ ~ ~ O ~ ~ earn IJI IJI JI IJI n O O O OOOO ~ ~ ~ ~ k k ~ k ~ ~ k ~ k ~ ~ ~ ~ ~ Cl O lh ei Ih Ih IA rh IA IA IA' N ~ ~ I I I I I I I I I ~ I I I I ~ ~ I I I I I I g 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 OOOO 00 f~ k k k k k k k k k k k k k k k k k k k~ kt k k~ k~ k k ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0 0 Cl 0 OOOO OOOO aooo 0000000000 OOOO OO ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ kkkk ~ ~ ~ ~ ~ ~ nnnn nnnih ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ IJI IA ~ ~ ~ ~ ~ ~ ~ ~ Irl IJI ~ Il Iri IJI lrl III IJI ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 8 IJI III IJI IJI IJI IJI H IJI YI IJI IJI IJI ill 4 'l 1g ~I &i; ~ .re 0 I STONE B, WEBSTER ENGINEERING CORPORATION CALCULATION SHEET L 5010.55 CALCULATION IDENTIFICATIONNUMBER J.O. OR W.O. NO. DIVISION 6 GROUP CALCULATION NO. OPTIONAL TASK CODE PAGE E/ /2/77, 3 f Af p(<) f'P'- @OIJ'g o g AT7AC.Hw e~ 7 e Co& pwR(Sou aF'QEssugg Resf o~sE sp&cvR+ ILII-'Trl I.C Tlq C SE66 &T. IO l2 l3 l4 16 I8 l9 ao 22 23 24 2S 26 27 28 29 30 3I 32 34 36 40 4I 43 44 4S 46 ~ l 4 E E 'IEEg~g IE I ~ $ Q P E E AI EE%.E E -I ~ ~ A II F' ISA) 0 AMPLIFIED RESPOND ~ SPECTRUM lge l986 '60 AUGUST 0 ON%'ING F LE 0038 5d j 8 l10 I' ~ H 30 I zo d 1C- ig >0 0. 10 ~ 10 i 10 ~ 10 3 Ru~ 3 FREOUENCY ( HE ) I D- l5 5<c .1 ~ ~- I I ~ / .ll ~ s f 1 Figure A-1 Pressure Response Spectra for the BCP Time History Selected {':'s g ~ ~, $ Ll for 4TCO Run 3, 5 to 7 Seconds. ~ I (. >> - ~ PPoM REF. l I 1 Pl ~J' ~ ~ ~f QA h F $ s,' RNPL IF IED RESt u i~ SPECTRUM aesr IS. ass 60 0 K 1 NN llO LK lO 8 QO 3' ~ ml ? 30 7) ~ gl 2. A1 n 0 10 C I 0 10 10 i 10 s RuN + to-l2 sac.. FREOUENCT ( H2 ) ~ ~ Figure A-4 Pressure Response Spectra for the BCP T)me History Selected for 4TCO Run 4, 6 to 8 Seconds. F'f20+ /zc r l'o ~ I > '2~ <<K ~ p f 4C ~ 1~ 1 tel ~ .I g 8 e t f P')$ t( ~ V/. \ RNPL IF IEO RESF PECTRUH AUGUST l9e 1986 0 E 1 MWHG LE lN 13 I n 7 rr Ol n 0' 0 10 i 10 i ( HZ ) PUN (D Sa<'REQUENCY 2o -zx F)gure A-12 Pressure Response Spectra for the BCP Tkme fl)story Selected for 4TCO Run 10, 26 to 30 Seconds. V.')~ b t ~A Nj 4 l 0 r f, f RVPL IF IEO RESPQi CTRuN AUQ5T l9s 1986 LI 0 E 1 SH'05 F LE Ol58 8 QQ 3D 20 I 4l p'o 0 10 ~ 10 10 I R~~ )~ ~4=275 c FREOUENCY I HZ ) Figure A-16 Pressure Response Spectra for the 8CP Time History Selected for 4TCO Run 15, 29 to 48 Seconds. ~~ J ~l C Feb. 12. 1987 To . N. Durka / T. L. Wang (Stone and Webster) .From . /S. Mintz (General Electric Co.) Subject Transmittal of Data Tapes for CO Load Def ini ti4TCO on Raw NMP2 The enclosed tapes contain the raw 4TCQ pressure data for the 4TCO runs identified in the NMP2 CQ load definition. For each of these runs pressure data begins at 0. seconds. and end well beyond the end times defined for the load definition time periods. Additional tapes would be req'uired to send the total recorded data for these runs. To e:<pedite transmittal these were not included, however necessary these can be provided upon request. if The CO load def ini tion f or NMP2 has been redef ined, elinminating Run 21 which included chugging pressure data. Additionally the load definition time periods with associated pool temperatures higher than 1~0 F have been identified. Table 1 contains the NMP2 CO load definition time periods. The time periods contained in the transmitted raw data tapes are given in Table 2. The CO data is written in 9-track, 1600 BPI EBCDIC f ormat. there are 5 tapes, the contents and attributes are given in Table 3. There are two end of f i le marks (EOF) at the end of each file. Each data record has a format of 2E15.7. The f irst word is time, the second word pressure. Each data record occurs at .001 second intervals. Contents> Table 1: NMP2 CO Load Def inition Time Periods Table. 2: Time periods in tranmi tted tapes Table 3: Contents of EBCDIC tapes First 0.05 seconds of data for each run on file Fi ve tapes wi th 4TCO data S. Mintz Plant Analysis Services (GE) 0 TABLE 1 Bounding Time Periods For NMP-2 CO Load T It'1E PERIODS (SEC) 03 05-07~ 12-15, 16-18 04 06-08, 10-12 05 19-21 07 12-16@ 18-21 05-07 09 10-13 10 20-22, 26-30 12 17-21 14 25-35 15 25-27~ 29-48 22 11-13 23 05-07 24+ 06-10 4 27 12-18 28 12-14 one scco~8 addi~c,q~l cLa ~a. o 4 e t' p~ I ~ iSO T4BLE 2 Transmitted Time Periods for NNP-2 CO Load TINE PERIOD ( SEC) 03 0-30 0-33 0-40 08 0-32 0-33 0-33 14 0-40 0-60 0 33 23 0-32 H 0-33 27 0-33 2B 0-33 4 I e TABLE 3 CONTENTS OF ERCDIC TAPES REEL FILE RUNS TIVES (SEC) 47190 0-30 4 0-33 5 0-33 02200 0-40 0-~2 0 33 41602 1 10 0 33 2 0-33 3 14 0-20 4 14 20-40 43303 15 0-30 15 30-60 0-33 28624 1 23 0-32 2 )4 0 33 27 0 4 28 0-33 + .I T 01 02- '3.035 SUNNARY OF CONTENTS FOR VOI'0 TABLE 3 FILE I I I'UNK VSN 40204 RECOh~.I& NKDIUM 9-TRACK CONTENT 4TCO RUN 03 0-30 SEC LABELS NONE OKNSITY, brl 1800 CHARACTER SKT KBCDIC LOGICAL RECORD LENGTH, SYTES 80 BLOCK SIZE, BYTES 1600 NUNBER OF LOGICAL RFCORDS 298V6 NUNSKR OF BLOCKS 1494 KOF FILE 2 I I'IPUT VOLUtlK VSN 38041 RECORDING NKDIUN 9-TRACK CONTENT 4TCO RUN 04 0-33 SEC LABELS NONE DFNSITY, SPI 1600 CHARACTER SET EBCDIC LOGICAL RECORD LENGTH, BYTES 80 BLOCK SIZE, BYTES 1600 NUNBER OF I OGICAL RECORDS 32864 NUNBKR OF BLOCKS 1644 KOF F ILK 3 INPUT VOLUNE VSN 38971 RECORDING NKDIUN 9-TRACK CONTENT 4TCO RUN 05 0-33 SEC LABELS NONE DENSITY, BPI 1600 CklARACTKR SKT KBCDIC LOGICAL RECORD LENGTH, BYTES 80 BLOCK SIZE, BYTES 1600 NIJNBER OF I OGICAL RECORDS 32864 NUNBER OF BLOCKS 1644 EOF KOF ~ ) 4,r I93r 01 0. 15.556
- 3) 0$ .l . '.00 . +$ .00 206.00 3+0 1JQ 206.00
SUMMARY
OF CONTENTS FOR Vl'00
~ <~. I ~ TABLE 3 Flu I s... UT VOLUME VSH 36183 RECOttOI HQ MEDIUM 9"TRACK CONTENT 4TCO RUH 07 0-40 SEC LABFLS 'NONE DENSITYI BPI 1600 CHARACTER SET EBCDIC LOGICAL RECORD LENOTH, BYTES 80 BLOCK SIZE, BYTES 1600 NW%ER OF LOOICAL RFCORDS 39835 NIPKER OF BLOCKS 1992 EOF FILE 2 INPUT VOLUME VSN 47049 RECOROIH0 MEDIUM 9-TRACK CONTENT 4TCO RUN 08 0-32 SEC LABELS HONE DENSITY'PI 1600 CHARACTER SET EBCDIC LOSICAL RECORD LENOTH, bYTES 80 bLOCK SIZE, BYTFS 1600 HUt%ER OF LOOICAL RECORDS 31808 NUI%ER OF BLOCKS 1594 EOF FILE 3 INPUT VOLUME VSN 48940 RECORDINO MEDIUM 9-TRACK CONTENT 4TCO RUN 09 0"33 SEC LABELS NONE DENSITY, BPI I 1600 CHARACTER SET tt EBCDIC LOGICAL RECORD LEN0TH, 891 ES 80 BI.OCK SIZE, 8YTES 1600 NQ'UEII OF LOOI GAL RECORDS 32835 I . ~ NUt%ER OF BLOCKS 1642 0O I~
..:I. I.'.,jf:;;, I; 0 t.-; ',::f,>> '. ~ .Qn 1
TABLE 3 541ST 01 18. 799 SmWARY OF CONTENTS FOR 3 41602 FILc 1 INPUT VOI.UHE VSN 39153 REroRnl m NEnI UH 0-TRACK CONTENT 4TCO RIIN 10 0-33 SEC LABELS NONE OEHSITY, BPI I600 CHAPACTER SET EBCnlr. Loolrpl. RLc"Rn LErNTH, BYTEs SO BLOCk: S I ZE, B TES i 1800 HU.eER OF I'.rolrai RECORDS 39835 HLkeiR GF B< oa".KS 1992 EOF FILE 2 INPUT VOLUME VSN 36803 RECORDING IIEQI UH 0-TRACK CONTENT 4TCO RUN 12 0-33 SFC LABELS HONE DENSITY, BPI 1600 CHARACTER SET EBcnlc LOOICAL RECORD LENOTII, BYTES 80 BLOCK SIZE, BYTES 1600 NLXIBER GF LO31CAI. RECORDS 32864 Ntl%3ER OF BI.QCKS 1644 FILE 3 I NPUT VOLLIHE VSN 33588 RECORDIN3 NEDIUH LABELS DENSITY'PI CHAftP Cl'Ef: SET f 0-TPACK NONE 1600 EBcnlc CONTENT 4TCO RUH 14 0-2P SEC LOAICAL RErGRli LEHOTH, BYTES 80 BLOCK SIZE, BYTES 1600 HUNBER OF LiGOICAL RFCORDS 19918
'NUIIBEII OF BLOCKS 096 INPUT VOI.Lk1E VSN 42405 0-TRACK COHTFNT 4TCO RUH 14 20-40 SEC EU . HONE 1600 c SET Ebcnl c t".COIIn LEIIOTII, BYTES 80 E, bYTES 1600 l:j'y , 'f':Lor.ICAL RFcoRns 19917 ;I)",g I .+l~'~i" 'Kl,'I q. Ill BI.OCKS 996
I 5407T 01 '7 F I a. RECORDIHO HEDIUH 16.579 SUHIIARY OF CONTENTS FOR 9-TRACK 1 4 43303 INPUT VOLUHE COHTEHT TABLE 3 VSN 14919
,4TCO RUN 15 0-30 SEC AOE LABELS HONE DENSITY, BPI ~ 1600 CIIARACTER SET EBCDIC LOOICAL RECORD I.EHOTH, BYTES 60 BLOCK SIZE, BYTES 1600 NIP'HER OF LOOICAL RECORDS 29676 NIGER OF BLOCKS 1494 FILE 2 I NPUT VOI.INE VSH 20233 RECORDINO HEDIUN 9-TRACK CONTENT 4TCO RUN 15 30-60 SEC LABELS NONE DENSITY, bPI 1600 CHARACTER SET EBCDIC LOOICAL RECORD LEHOTH, bYTES 60 BLOCK SIZE, BYTES 1600 Nlk!BER OF LOOICAL RECORDS 29876 HWRER OF BLOCKS 1494 aEOF PJ I FILE 3 INPUT VOLUNE VSH 34901 I RECORDINO HEDILN 9-TRACK CONTENT 4TCO RUI'I 22 0-33 SEC I LABELS DENSITY, BPI . ~ NONE 1600 ! ',' I CHARACTER SET EBCDIC LOOICAL RECORD .ENO)H, BYTES 60 BLOCK SIZE, BY'IES 1600 HUNEKER OF LOOICAL RECORDS 32664 HUIAER OF BLOCKS 1644 EOF
~ I (t(N, g
- if>. t'I'IIt't 3.
~gL sit - q '.1~" it
~ 'I ~
pFg w 1'e@'
TABLE 3 5432T 01 i 7 18 996
~ SINHARY OF CONTENTS FOR V 28624 Flu 1 INPUT VOLUHE VSN 08062 RECORD I NS NEO I IN 9 TRACK CONTENT 4TCO RUN 23 0-32 SEC LABELS HONE DENSITY, BPI ~ 1600 CIIARACTER SET EBCDIC LOGICAL RECORD LEHSTH, BYTES 80 BLOCK S I ZE ~ BYTES 1600 NUHBER OF LOSICAL RECORDS 31868 HIPSTER OF BLOCKS 1594 FILE 2 INPUT VOLINE VSN 42758 RECORD I NS IIED I IN 9-TRACK CONTENT 4TCO RUN 24 0-33 SEC LABELS HONE DENSITY'PI 1600 CHARACTER SET EBCDIC LOSICAL RECORD LEHSTH, BYTES 80 bLOCK SIZE, BYTES 1600 NUHSER OF LOSICAL RECORDS 32864 'I 644 NUI%ER OF BLOCKS EOF FILE 3 INPUT VdLUNE VSN 47690 RECORDINS HEOIIN 9-TRACK CONTENT 4TCO RUN 27 0-33 I SEC LABELS HONE DENSITY, BPI 1600 CHARACTER SET i EBCDIC LOOICAL RECORD LENSTH, BYTES 80 BLOCK SIZE, BYTES 1600 NUHBER OF I.OSICAL RECORDS 32864 SN NUHBER OF bLOCKS 1644 EOF FILE 4 INPIIT VOLINE 03172 RECOROIHS NEDIIN 9-TRACK CONTENT 4TCO RUH 28 0-33 SEC LABELS NONE DENSITY, bl'I 1600 CHARACTER SET EBCDIC LOSICAL RECORD I.ENSTH, BYTES 80 BLOCK SIZE, bYTES 1800 HW%ER OF LOSICAI RECORDS 32864 NUHBER OF BLOCKS 1644 EOF EOFa C
'4 + + AL ..( ST 01 02 13. 035 VOLlNE 47190 FILE I 4TCO RUN 0 EC 0 IlUN 03 I. SKC Oo 1103985K 01
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