Design Report #7 B&W Contract No. FORINORMA7ON ONLY · composite transient curve developed for the cold leg fluid and the make-. -up fluid. Of primary importance was to select transients

0 SC 15 23 Design Report #7

Thermal Mechanical Stress Analysis

of

High Pressure Injection Nozzle

B&W Contract No. 620-0003-50 Customer: Duke Power Company

FORINORMA7ON ONLY

Prepared By:- W.L. Tankaley and Associates, Inc.

Reviewed By:

Approved By: /).7 =

Report #7 - "Thermal Mechanical Stress Analysis of High Pressure Injection Nozzle"

Replace entire report with the "Thermal Mechanical Analysis of 2-1/2 Sch 160 make-up and High Pressure Injection Nozzle" for 620-0009-50 as modified in FCA 04-3601-00 (Reference #4), B&W Document 32-1128224-02 (Reference #1), and the changes to the 620-0009-50 report described below:

1. Page iii - Reference A.1 - 150156E-6 should be 131924E-9.

2. Page iii - Reference B.1 - Add "As modfied by FCA 04-3599-00.

REV DATE

970514031F 970508 PDR ADOCK 05000269 S PDR

REVISION PAGE

R EV. B NO. PAGE DESCRIPTION DATE

ALL INITIAL RELEASE

The changes below indicate the modifications required to update the 620-0008-50 analysis to the requirements of 620-0009-50.

i Added last sentence in Scope.

Changed 70o -9oF to 70 0-95 0F in 4ti line of Discussion.

Eliminate all but 1st sentence in Conclusion.

. ii Omitted primary stress results in Results

0 Section. 6-73 FLB/

iii Reference A.1 revised for NSS-9 contract.

Reference B.1 revised for NSS-9 contract.

1.0 Added explanation for a dimensional change on nozzle.

1.1 Added NSS-9 dimensions (asteriked) to nozzle sketch.

3-56 Add statement at bottom of page.

3-65 Omitted Case-2 earthquake loading.

3-66 Omitted all reference to piping reaction stresses..

5-21 Omitted all references to earthquake loadings.

5-22 to Omitted all reference to piping reaction 5-31 stresses.

ii Added note referencing fatigue analysis 5-21 with pipe loads contained in Section nF".

1 5-24 10/29/73 DMcK/i3

5-25 5-28 5-29 5-30

5-31

Revisions For ES:- Reoort #

Date age Revision Comments By

0

'*..

0

*

INDEX

Page

Scope, Discussion, Conclusions ..................... ****** ****...i

Results ........ * * * * * * ** * * * * * ** * * * * * ** * * * **.

References ...... ******* *********************** ***** *

Section I

Geometry ............ ** * * * * * * * . . . . . . . . . . . . . .Stress Concentration Factors .................................... 1-2

Section 2

Temperature Distribution of Make-up Nozzle ................... 2-1 to 2-29

Section 3

Stress Analysis of Make-up Nozzle ................................ 3-1

Section 4

Temperature Distribution of HPI .................................. 4-1

Section 5

Stress Analysis of HPI Nozzle .................................... 5-1

17)1

, SCOPE:

This report contains the Therma./Aechanical Analysis of the makeup nozzle and high pressure injection nozzle. These nozzles have the same geometry but are used for different purposes. They are located in the cold legs on the discharge side.of the pumps& This report contains

the justification of primary plus secondary stress limits and the fatigue analysis as defined in B31.7 "Nuclear Piping Code". Satisfaction of basic pressure sizing criteria and reinforcement calculations are found in Report 1 "Code Sizing Calculation". Piping reaction loads and stresses can be found in Report #4, "Piping Reactions".

DISCUSSION:

The make-up nozzle and high pressure injection nozzles have the same pressure, branch momeint loading and run moment loading, but have different temperature distributions. The make-up nozzle is predominately cold in that it has a fairly constant flow and is at a temperature of 700-950F. The HPI is only used for a sudden pressure drop condition, and thus is at a temperature consistent with the cold leg temperature, 5500-5750F, when it is shocked with 60oF water. The critical stress location in the make-up nozzle occurs near the nozzle to run pipe.intersection whereas the critical stress in the high

7 pressure injection nozzle occurs outside the thermal sleeve in the upper part of the nozzle.

The analysis has essentially the same format for both nozzles. First, the temperature distribution is evaluated for various transient conditions emand time-temperature plots for-selected nodes are made to select critical times. These times are then used to calculate stresses, and thus stress ranges can be determined for thermal stresses. .Secondly, stresses are calculated for pressure loading, and the stresses are then combined to obtain the total stress picture. Finally a fatigue analysis is performed to demonstate acceptable performance during the.design duration.

CONCLUSION:

The make-up nozzle and high pressure injection nozzle meet all the requirements of B31.7 1968 Draft.

* IP

RESULTS

Primary + Secondary Stresses

Branch Intersection Make-Up Nozzle

S =21.1.ksi < 3 Sm 53.4 ksi

End of HPI Nozzle

S = 107 ksi >3 Sm = 51.3 ksi

An elastic plastic analysis was performed. Range of primary + secondary stresses'occurring more than 250 cycles.

S = 9.85 ksi < 3 Sm.= 51.3 ksi

Fatigue Usage Factors

Branch Intersection make-up nozzle

U= .045 1. 0

End of HPI Nozzle

U= .953 <1.0

N(TE: This fatigue analysis includes thermal and mechanical discontinuity stresses only. For inclusion of stresses due to run and branch pipe motions, see Section "F".

C)

to/9173

ii

REFERENCES

A. Drawings

1. Babcock and Wilcox Drawing 150156E-6 "Assembly and Detail for 2-1/2n Pressure Injection Nozzle"

B. Codes and Specs.

1. General Functional Sppcifications for Reactor Coolant System Components, CS(F)-3-92/NSS-9/0372.

2. Nuclear Power Piping, USAS B31.7, 1968 Draft.

C. Computer Programs

1. 91167 - "Temperature Distribution"

2. 91032 - "Temperature Interpolation"

3. 169 - "Ring Thermal Stresses"

4. 91079 - "Thermal Stresses and Motions from a Radial Temperature Z Gradient In a Long Cylinder, Short Cylinder, or Spherical

Segment"

5. 91191 - "Annular Plate Thermal Motions"

- 6. 91060 - "Interaction Analysis"

D. General

1. Tentative Structural Design Basis for Reactor Pressure Vessels, U.S. Department of Commerce, Office of Technical Service.

2. Stress Concentration Design Factors, By R.E. Peterson, John Wiley and Sons, 1966.

SECTION 1

This section contains a sketch of the make-up nozzle (identical to high

pressure injection nozzle) demonstrating dimensions used in the analysis.

This sketch appears on Page 1-1. The dimensions with asteriks are those for

the NSS-9 nozzle, which are different from those analyzed. The change will

have little effect on the final stress results. This reasoning is justified

by a review of similar geometry nozzles, using the dimensions with asteriks,

which were analyzed for similar thermal transients. The results indicate

that a small change in piping dimensions have a negligible effect on the

stress levels. The ratio of actual stress to allowable stress for the

nozzle to pipe intersection is 0.395 which allows for a reasonable increase

in stresses due to a change in geometry.

9 Stress concentration factors are also determined in this section.

1.0

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2STRESS CONCENTRATION FACTOF

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BABCOCK'08& WILCOX REVIS ION

DEPA~RTMENT ______Z__7_-_-7___

ICHFCKFD DATF E

OSC 1522 SECTION 2

This section contains temperature transient analysis of the make-.

up nozzle. A survey of the functional specification was made and a

composite transient curve developed for the cold leg fluid and the make-.

-up fluid. Of primary importance was to select transients which would

reflect maximum temperature differentials in the nozzle. This differential

is dependent upon temperatures of the corresponding fluid, rates of change

of the fluids, and flow rates.

The make-up nozzle has two predominant temperatures 950F (normal

operation and essentially constant for all transients) and 70oF (For the

feed and bleed operation). It has a predominant flow rate of-13 GPM but

can go as high as 100 GPM1 or as low as 1.5 GPM. In particular it has a flow

rate of 40 GPM during feed and bleed when the fluid temperature is 70'F.

The cold leg fluid goes through several changes in temperature but

the most predominant temperatures are 555 0 F for 8% and 100% power levels

and 5750F for 15% power. The temperature does go as high as 590 for the

reactor trip.

Consequently the temperature transient curve was made to reflect these

variations in fluid temperature and flow rates. The pictorial diagram is

shown on the following page.

IN.

FOR, Fil C4

/f/z , I q ly--

.QS C. F114 COEFFICIENTS

The film coefficients will be calculated assuming turbulent flow in

the cold leg and nozzle. They are calculated for three different cases:

1.) in the cold leg 2.) in the branch pipe and 3.) within the thermal sleeve

because of the smaller diameter. In addition the small area of contact of

the fluid with the nozzle on the inside of the thermal sleeve ring (see figure

on Page U3 marked Section 3) was assumed to have a film coefficient of 200 BTU/

2 HR-oF-Ft. when there was a flow in the cold leg run pipe and 100 when there

was no flow in the run pipe. The' 100 BTU/H-oF-Ft.2 value was also used as

a natural convection value for the run pipe (Cold Leg) when there was no flow

C0 during cool-down when decay removal starts.

The film coefficient for no flow in the nozzle was assumed to be 35 BTU/

ir--or-Vt. 2 TLb bjualler value was chosen because of the smal.Ler diameter and @

that the water would be closer to stagnant within the nozzle. The thermal model

of the nozzle includes water blocks behind the sleeve. It is felt that there

will be little or no flow behind the sleeve because of the very small gap between

the sleeve and nozzle at the top of the nozzle plus the "Vena Contracta" effect

of the flow going from a larger diameter to a smaller diameter at the transition

from the branch pipe to the nozzle. Thus only conduction is assumed between the

sleeve and the inside of nozzle. At Section 4 metal to metal conduction is assumed

but a contact resistance coefficient of 100 BTU/HR-oF-t. 2 . This value results

in essentially metal to metal conduction. The rolled-in portion of slecve is assume

to have metal to metal conduction even thougha-s!nall gap may exist at certain ti.eF

within the transient.

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I1.

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,x.' tiJ. -HJ'A

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FILM COEFF!C ENTS

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Lbs/FT-rR G-AL./MIN GO MIN/ RfS.3*9 7 Lbs/G-A.L)/APE A

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C! 7 77 00 Q Y 0 c,p M x 4 .l oo9. .s F H

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Zu~ izVE Zi0O urrzc- 9A.T +1

150 TERIPrRATURE DISTRIBUTION

The temperature distribution of tiie nozzle was obtained using B&W

Thermal Program 91167 which performs a transient temperature distribution

by solving internally generated heat balance equations as a function of time.

The grid for this program is shown on Page 2,-8 and the computer output

which follows depicts the input items. A heat balance equation sample is shown

on pages

Pages -Cop.ashow a graphical representation, temperatures vs. time, of

C) selected nodes and this is finally followed by the computer prirt-cut giving

the actual temperatures at the selected critical times for stress analysis.

C

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0 7 5 l *0 .1 7 4 ? 0 3 t 6 9 . 1 t . 01 6 9 4 * 2so

0~~ 77 i*s .9b 0l *01 b * 17ol 7*l o l

0 69 l * 14 43 *032 (0 *18 96 .032 79 .116 3 0 70 14 . / 4 .009 *71 178 .009 00 .110 b0

o 70 1.0

1 14 4- .f ? 1 .9 / 90 1 0 71 . 1.0 U .114 416 . 00 (3 .18 9h .009 / 60 /

1 72 1 .0 74 b 9) .U 2b2 73

0 73 1.o .1(14 471 .0u10 74 17 99s10 .01S *13 ...

0 74 10 u 114 49 .018 15 1 100 .15 t 3 74i 6 /4? 7

0 75 1. .1UI1Y4 49. .Ol it d1/ 10 0' 4 2.

0o 7 1..1 14' bO .021 . i7 .its 102 *.'18 e /5 *t09

0 776 1 0 ?u SI. 13 . ta .'I. 103 .011 16 .1 ~ 77 *

0 78 1.0 .80 52 .016 79 .~.4 .0 / /7 0 1

0 7 9H 1 .0 : ? 0 3 . - 0 o 41 1 05 In 6 S *1 ts .12

o 70 1. .2bC U4 .3 1 ..4 ~ 02 7 .116 ho

o. b1 10. 0 54 .032 81 107 .032 0icj h

0 83 .J .0 / 0 89 tob ,0 .01.1 82 76 8

0 aas .I .U1 0a 8.4 11 08 8 13 0 ab 1. *210 uV9 .01 1 .j . * 111 .008 - 04 .159 d

0 86 l.u .280 60 U6d t? *541 112 .041 6i5 *0D h6

o 87 1.u .280 1 *C1 Md *Stl 113 .Inb bb, .015 81

0 8 1'.0 .2.110 6? * ) i *541 114 ,bb/ 87 .013 1 i

0 89 1.0 *280 63 .05(1 90 .541 115 .050 8 .Oa 9

0 90 1.U .2d 64 .0 i, 197 *541 611 .1050 9 .062 90

o 1 1.0 * 154 bS . .002 b2 .34 91

o 9? 1.0 *6 06 .1u5 93 .003 9I .b39 92

0 93 1 .15l8 6 .022 94 .;11 92 .810 93

o 9** 1.0 *lba 68 .0S ; L .0*4 93 .703 94

095 1.0 .1a 69 .009 ' 9 .113 ill .01.i3 94 .702 95 .

o 96 1.u .Iaci 70 *OU9 97 *118 11. .009 95 .106 96

0 97 1.0 *Ibi 71 .009 9H *118 119 .009 96 ./06 91

0 98 1*u * hib ? . 009 99 .118 120 .009 9. .760 c:0i

0 99 1.0 .156 73 . 010 100 .118 1 .00s 98 .105 99.

0 100 1.0 *5l /4 *ld 101 .118 122 .Oib 99 .692 10)

0 101 1.U * 8 15 .01t 102 .118 12i .014 100 .009 Ini

I1 12? 1.0 *1Sa 7e- .021 10.3 .118 12L. .014 101 .680 102

0.7 .01.5 10-* ' 1?5 *011 102 .146. 103

o 104 1. . . 8 I .010l 126 .013 103 -.134 104

0 1.05 1 *478 79 .03d 106 .350 12 *?5 14_ .107 1j'

1 615 1.0 *4/li 80 .0 2 10/ *iud 128 .032 105 *300 306

i0 107 10 8 1 .032 10h .3 19 .12 106 .100 101/

04/,. b? .021 10J .9568 130 .032 107 .111 108

0 19 1 .478 b3 .00 11 .3Io3 131 .011 10)8 .14 109

0 110 1.0 *.4/i . .00s 111. . 3b 132 .008 109 .14, 110

0 1 141 k .012 112 .JS 133 .0)6 110 .144 11 0 11l 1.0 *4/c 86 .*088 113 .458 134 .001 lil .035 13 1

0 113 .0 . 1 .076 114 .30 13s . 6 6 112 -. 000 113

0 1 1 .0. .4/ Id .050 115 .355 136 .051 113 .Ub/ 114

0 115 1 0 4/h t 14 .U u 11 *1 tL5 137 . .050 114 .0o'i 115

116 1.0 *4(8 90 .064 197 .isH 13 .0. 15 .046 1bi

0 117 1.0 *0:0 9s .009 118 .9"11 117

0 114 1 *050 9. .00 119 .u0 1 .932 118

o 1 19 oil .050 91 .0069 1?o .009 11 . t11s

o 120 10. .50 98 .009 121 .009 119 0*J? l0 121 1. . 0 99 *010 12 .00 120 .9.10 1,1

0 122 1 U.050 10) .016 1e3 *015 121 .-fl/ 12

3g 0

1? .01A iuj,-> U 1 1 ?_ .9 11 1 4)

o 125 .0 .153 ~0:1 .13 1"/'''aL I I1/4i '.8 , 0 12- .*0 .153 10'. .010 i?, .013 125 .818 12

0 1P7 I 1.0 .153 10 . .032 126 .025 126 .7 1 121

0 128 1.0 .153 106 .032 1 9 .130 139 .032 127 .654 128

o 29 1.0 .1b3 107 .034 13') .130 140 .032 123 .bs 29

o 130 1.0 *153 10A .021 131 .130 141 .032 129 .665 130

o 131 1.0 .153 109 .00t 13? .130 142 .011 130 .699 131

013 110 .t'08 133 .130 143 .008 131 .02 (32 0 132 1 * *153 111 .012 134 .130 144 .00t 132 .n98 133

0 134 1.0 .153 112 .088 13- .130 145 .041 133 .S1,9 134

o 135 1.0 1 *t3 113 .06 136 .130 146 .u1Wit 134 .S54 135

0 136 1.0 .153 114 .050 1 13 .130I 141 .05/ 13L . 2 136

0 137 1.0 *b 3 115 .0 t0 38 .130 148 .0 50 146 .619 13

o 138 1. 153 116 .060 1/ .130 149 .U( 1317 .601 1

o 139 1.0 .093 1211 .032 14J *t/ 139

-0 140 1 0 *)93 1 ,9 .032 141 1 150 .032 13) .139 141

0 141 1.0 *I) 3 130 .021 14? .1 0 151 - .032 140 . 49 141

0 142 10 093 131 008 143 .105 152 .011. 141 .84 142

0 143 1.0 *193 8 32 00 14'. 10% 153 .008 142 .1l. 143

o 143 1.0 *1)93 133 .12 i45 *105 1'4 *00b 143 .732 144 0 144 1.0 -.1 93 1U, .0. * 1-6 .'* 5 1.5 .041 144 .t 3 I

0 145 1. .093 135 .00B 141 .10. 156 *0U8 145 .6Th 146 0 146 1.0 *(93 136 .01b 148 *10 151 .0b1 146 .696 197

0 147 *0 1 *93 137 .00 149 * 1 'o .Ub( 147 ./03 148 0 149 1.0 *o93 137 .068 197 *105 SY *050 147 *68b 19

0 10 1.0 *1M 140 .032 11 *98. 150 0 150 1.0 . .901 141 .021 168 *103 100 .032 150 *150 151

0 151 1.0 *088 1'2 *000 153 *103 161 *011 151 .790 152 0 153 1.0 *0*t 143 .0?o 1M? .103 162 *001 152 .792 153

0 1S3 1.0 *o8. 14q *012 15 .103 163 .008 153 .7 9 U 14 0 15 1.0 *0b 145 .018 156 .103 164 *041 1 4 .679 155

0 156 1*U .*38 146 .u76 151 *103 165. .0b 155 .649 156 o 153 1*0 *0td 141 .0o A .13 166 .57 156 .7 2 157 0 1 1.0 * .8 .148 .050 159 .103 16/ .050 157 .71)9 18 . 0 15A 1.0 * 149 ,Thn 191 .103 16b .050 18 .691 159 o 16 1.0 0119 151 *021 1 1 *884 160

0 161 1.0 .*089 15? .0(U I). .102 169 *011 160 .790 1o1 0 162 1.0 *019 153 *01 163 .10 1(0 .0 1b1 .792 102

0 162 1.* ..*89 154 .012 11.4 .1)2 1/1 .00U 162 */8c I63 0 163 l*U

0 IA4 U .89 1 1.2 172 .041 113 .6.19 164 0 165 . -0 ut e O .3021 wa .tr8 *l14 .0844 10

o 16. .0.89 17 .00 li .1o2 174 .ub5 1b5 .702 166 0 167 .0 .049 1 00 1s .10? 175 .Ou 166 .709 167

0 1AA l*u .089 159 .0n6 197 .102 176 .050 1/ .691 168

0 1 - 1.0 .119( o t 6006 110 .902 1o9. o 170 1.0 .(190 10n . .006 1 /1 . 0i) 1.- .894 170 0 171 1.0 - .090 163 .01d 11? .00 110 .590 171

0 17? 1.0 .090 14 . 08 1/3 .OU 177 ..041 1I .690 (2

0 173 1.U .090 165 .u7 14 .05 175 .10i 172 .661 1(3

0 17. 1 . .090 the) .Ou 1/b .U11S 179 .051( 173 .719 /4

0 175 l*J *,90 It7 *050 el tUbb 180 .00 114 .126 0 1.76 *u .190 16 .608 197 .tj A 181 .u0u 175 .708 i 16 0 177 1.0 .03 172 .03 17. .043 182 .816 1

0 17R A . .w33 17,1 .016 17P .093 183 .dd 171 .7t0 1 78

u1 0 *Sb3 1(4 .fit)0 1io .'s. J 114 ."057 17I .798 119

0 10 1.0 .053 176 .050 1:. .03 18, .0u 14/9 .8t 10

0 1h1 A *1 *053 176 668 I197 .U43 180 .0Ou 180 .707 B 7 I

0 1i2 1.0 .0?2. 177 .08H 18.1 .021 187 .fiH I2

0 1A3 1.0 .024 178 .07t 18, .021 IBM .i0 h1 .792 181

o IP4 .0 .024 1'9 .00 lb .uL 1i9 .057 183 6649 LA54

0 15 1.0 *d4 1an .05t 186 .021 1 .U 180 .856 1H5 0 186 1.0 .1)24 181 *O6 19! .ui1 191 .050 18i .83 1.0

0 1S7 1.0 .013 182 .Ohi 1 .1 .0U0 19? .891 10(

0 188 1.0 *013 183 .0 lt 1 .08 193 .08 18i7/ .m16 1a c) 0 .0, 1.3 1844 . 050 19 * M I9 *b3' 88 * 7.3 189

0 190 ) . .013 185 .050 1L1.1 00: 19 .050 15-a .880 190 0 191 1.0 *013 1b0 .u68 197 .008 196 .050 190 .862 111

0 192 1.0 *10? 187 . 086 193 .910Q 192 0 1(43 1.0 *00? 185 .070 194 .08 1 .834 193 0 194 1* .002 189 .0)50 I .V57 193 .891 194

0 195 1.0 *002 190 .ti u 196 .050 194 .h99 195

0 1 0 1.0 .002 191 .0 8 197 .L05 195 .880 196 0 197) 1.0 1.000 197 0 198 I*. 1*.o 0 19i

0 1i9 I.0 1.000 199 0 200 1.0 1.000 200

DELTA THETA =1.738E-04hRS/ITER hLOCm 113

0oo >

,IQ

02c 0 ( 0. 6 I 9 0--3 2

osIc 15 22

'2.I 0 LL

7.;

-001

600

OL

Vol

a

Ik.1

057 OI.

0OSC 1522

SELECTION OF CPITICAL TIMES

After a study of the precedinj graphs the following times were chosen

for stress analysis:

ITERATION (TI,.HS.) EXPLAATION

28169 (4.95) This reflects a time near the end of heat-up to 15. power and is essentially ecuivalent to one of the worst axial

gradient cases at 15% power.

41428 (7.5) . Steady state at 15% power. This reflects hottest cold leg temperature for a prolongec time.

52659 (9.66) Reflects steady state distribution at 8% or 100% power.

75168 (13.9) Reflects axial gradient at end of feed and bleed. W

86960 (16.099) Reflects maxim,= temperature of cold

leg when trip initiates.

103154 (19.2) Reflects short time after decay heat removal initiates and a reversal in axial gradient.

The stress analysis of these cases should define an assurance of stress

levels in the nozzle and ranges in stress levels such that fatigue criteria

can be Justified. This will be discussed further in the stress computations

portion.

1~. a6 r < a911S7 16 6 4* ,*1114 11 O910:,*- A J 1o3 100 s . 0 3 11 1.4 1 1 10if : ../. 2 0 s4 I 40 e I1 *3" 4*->7 I7 2 1 4.95009 19 112- 121 3.9 158 , j J1) 311 96 97 4.95(j9

219 81 4+5 .464 38i9 4?? '0t 24 232 261 293 32 4.950,09 2q169 91 97 99 7 141 -9 5 o w 16 1 1 81 20 2 3 1 10 1i 3 / 137 160 1.9500') ?P 'V 111 -+6 *U9 33 64 29 34A 3ob 391 424 4 .95009 e'. 1 )Sh 3'41) 183 24 10 10d 114 12 ' 131 .27. s 23i 294 328 351 370 4.95009

2?169 1.l 374 398 431 471 335 S6 4 4.95009 PA169 .. 1 72 401 43b / I -i 532 551 26 362 4.95009 ?H169 161 , 04 436 7Ii 1 3 4?,? 4561 40b 37 4.95009 2A169 171 480 425 534 (45 S74 Sol 07 309

6 1y2 9h 97 9 564 1 (A 5J2 51 560 4.95009 2P)69 191 572 S67 5b9 t* 631+.9$909

23. o J2 35-,0 4 5o

.8

** ): 2 5 9 55 3e 4900

11 lIts je 0 1,J3O 64. 9 i 3II, ?U 96 9 *"*(7 /21 99 If)' 109 IJ t i4 110 171 .1 196 214 (.10 6

* e2 I- .9t .9> 9b 7 000b *0 70 1 )9 9, 90 99 104 113 138 157 149 7.3isC6

0 700 5) ,06 269 '9 J343 36, 404 444 4 14 7.3 ij06 0 700 61 4i/ 49n m 46 'h6 54 ?h 9L 96 9 6 91 7.36C00 V700 71 100 10i 116 139 i!9 1113 2B ? 238 2/2 30.4 1.36006

40700 81 328 341 334 410 4b1 481 49 510 544 56. 7.360,i 40700 91 9b. b'j 95 96 9( 98 - 101 10/ 119 140 .7.36006 40700 101 161 180 E231 274 ' JO b 331 351 378 41. i.300ab

04)7(100 111 'b. ' .499 1l1 S44 504 97 98 101 3 7.( j6 40700 121 121 141 162 187 211 240 275 310 335 355 7.3600b

40700 131 362 418 460 +91 5 29beL 545 564 318 J'l 7.3,006 0700 i 's1 361 387 42? 466 4 0, 513 529 548 565 348 7 .36006

40700 151 A * 391 42o 471 bS S 1 535 551 566 J/2 7.36006 07 161 394 42 1 474 bl2 556 540 554 567 397 4:30 7.36C6

0700 17i 476 522 554 i 8 41 546 53 b6A 0 40700 18 570 555 557 561 b6 5/1 565 566 567 bl0 7.36u06

0700 191 573 572 572 573 S/3 5/4 S'7* 575 95 9!

41428 1 98B 100 105 u 101 163 - 106 109 113 116 7.50007 142P. 11 118 120 123 126 130 13.1 196 220 96 97 7.14u07

1 2 21 99 102 109 120 131 144 160 117 19 b 214 7.b0007 142 31 22.9 239 254 e/4 21 324 25 95 95 7. 0I 41 42 . 41 95 .S 96 91 99 104 113 138 157 179 7.50007

1428 51 206 235 264 299 323 343 369 404 .444 471j 7.S0007 41429 61 4.< 456 bL9 9S 95 9I6 96 96 7.50007

14?9 71 100 105 116 i39 119 1433 - 209 238 272 3U3 7.5:0007 T1?A R1 3?ti 348 3/ 410 451 4s1 491 - lu 544 565 7.50007 1428 01 9! 95 95 b '47 lI o 107 119 1 +0. 7.S0CU7

41 42: 1)1 .161 18L 210 239 2/4 J06 331 3t1 3/8 413 7.00 4142 1 111 4i5 485 499 hI t ble4 e4 V) 1 98 1(1 1t 7.5000/

41/2. 121 121 141 .16? 1h7 211 20 27 YS 310 335 355 7.L0oo7 4142. 131 3 ri 41A 460 491 bob 522 545 564 318 d 341 7.50007 41428 141 381 387 422 4e6 Aib 3 529 4 d 5tb 38b .5 007 41'28 151 366 391 426. 41l 519 S3 Sbt I66 3/2 7.5o007 414? 161 394 4?0 4+4 5i -- 2*0 554 561 397 430 7.50007

4142 171 ?4 52? 534 . .- 7 541 b-6 553 S61 7.5007 4142/4 131 570 S5 * 7 S .t1 S 57 57u 7.b0007 41428 191 73 ** 572 572173 511 b/4 5715 b/b 9S

' ;if/ 11 I/ 1 't. Io ;. I Iit 9 119 '.t 0 ( 0 9 )3 '*9. 91. '.' 1j9 t4 321 P i e . 1

50268 ~ ~~~ .'1Y.9 6s 0 .5 1 5 S9 9 ;j())196 9 99 104 1 1? 136 15S 176 9.20019 ;?1 . 314 333 3' 391 430 458 .20019 S 7i~8 1 100 O- 105 1 5. 131 15 p 1/19 204 23; 265 2 ( ?~U0 14 50268 71 310 33n 33 i7 436 45 47 4 93 b if 9 .200 19

S0268 9 1 295 9 96 96 98 101 106 118 138 9.20019 1015 158 181 P 8 u 233 2S96 2t 321 340 - 366 400 9.20019 5 A06 111 44Uo 4.69 -#82 4+Y8 5'S 97 983 1 (1 11 u .2)00f)19 502691 121 1e0 140 159 1k3 7u rj4 3011 7 344 9.20019 50n268H 131 X3?o 404 L#7 .4450 to .> 5 2#; s 'I t. 309 131 9.20019 50268 141 35 0 37S 409 41 4 1 O 1 5 511 59 14 331 9.60019 5r 26 151 32 379 412 45 502 516 53 546 33 9.?.19 50268 161 367 414 458 495 502 s4 6 535 54b 385 4 9.0019 Sl?69 171 3460 504 516 37 -538 49 52 527 533 542 9..20019 59268 181 550 536 5 3 e '.1 546 552 545 546 548 550 9.20019 .50268 191 553 658 54 S3 554 5h4 5558 1551 0 95 95

52659 1 91 100 104 100 101 103 106 109 112 115 9.b6003 52659 11 117 111 121 lis 1 ek IS3 143 2 1 96 91 9.66003 52659 121 39 3j 109 I19 1.0 12 b 7 113 192 209 9.66003 5?659 31 .22 L- 233.2.4 ts b7 2,)0 307 *315 25rS1 95 1> 9.6r.0u3 5c~ 41' 99 96 T/ 104 11 t2 55 1b .b(0 52659 1. 320 229 451 291 314 333 35 391 430 458 9.66003 9 2659 .1 '1 C;3 52 Li69 95 9 693 .6o 52659 11 100 105 5 127 156 1'9 514 523 5 95 . 9.62003 5659 11 31 338. 363 3; 7 43t, 45 4/S 4 v 5?5 515 9.66003 5.659 91 ti 9 95 6 9H 101 0b 11 13 9 S S 9 ?b5 9 101 158 1111 205 3j 3 'l 2 321 : U 366 400 9.66003 * .2659 111 4.40 46c; 482 41i8 no L 54!3 97 98 101 10.1 9,66003 * 259 121 .120 1( 1S9 183 200 eJ4 2$ 30 1 325 -1.' to4 9 .t)60 03 13 1 .-3 1 404 445 '1 S 410 ~0 & 526 545 309 3.31 9.66003 6. 9. 141 3150 .37h 409) 16 1 41s) 4 5i . 11 529 . 37 9."6h0 5,>65 151 3Sto 3/tQ 412 4t>5 48 f5 52 b16 532 546 3 bO 9.66U ' 3 C.69 161 3i142 414 458 4.95 56 535si 5483 3135 416 9.66003

*.5S9 171 146,. 504 516 527 53$I 4 52 527 533 .54 2 9.bbU03 f-, 9 l1 550 ti46 54b 54i 546 !it2 545' ~ 546 '8 550 9.66u03 Q. 2 %6 1191 54 552 .55i! 5 53 55' 55o4 5!55')SS 95 95

7;: 'st 17o2 1 /A .3 2I 9 .u1 1 0. 12 11 ~~L

5 o 7 1. 1419 4n? 13.9014 7 71 1 /i 1it t1 3o ( d 1 .900 1.4

7.1 39?0432 0 1.id 4 .r. 511 2 9/ 1 .90 1 4

.J4b J6 4 0 I4 'A 4?i? 4 2 to 4J Let ?

7'7 164 -13fo y -/0 4 32 547 111..9004

751 63A 101 b43 5151, 1833 .124 24/ 1 1 1 .90014 7516 Il 34 45 3 3) 388 15.30 17

I 9 11 13 4 -3 1 1 12 194 5? ? 1 .001 7 1 8 11 17 3 2 130 12 164 ? 24A 2P-4 30 1 39 14.0017 7?5 9 ~ 13 361 39 02 544 2i 329 13.9 0014

75,815 392 401 506 546 54 32219201

96 97 10037 130039 102 104 194 .15000 7

361 31 211 22? 23' 2' 2'* S 300 I 5 9 9 14.00017 31 95. 95 9 6 97 . 107 12 146 16 1 14.00017 ..4191 21S 2u 279 31 J< 34 34 473 452 14.00017 77 171 464 47 525 5 b24 . 59 6 114.00017 795 101 110. 129 347 10- 193 2i 23 25h3 514.0017

Th 7~ ~1 30/ 327 3s3 3til '.29 - 1 4/3 Ldts 523 544 14.(:0017 795 95 0 9 b 97 99 102 112 130 14.00017 7 1 1 149 Ill 194 222 25b 0 31 329 35b 391 14.00017 0E7~o 1.1 433 . 162 477 4w. 59 98 103 14.00017 7 lb 113 131 150 172 195 2.:'2- 25( 290 31. 333 14.00017 S 131 340 395 43 - 419 .. + bt 54 544 29/ 320 14. 00017 7' 1,1 39 ; 400 6 77 4'.1 I0 52146 321 14. 0001 ?b0 151 4u3 i. 13 b 5 3s9 14. 017 5 0 11 32 406 452 491 Sub S .- bd3 b 375 407 14. )0017 757,0 171 44 404 513 525 9S3 5 L 2 5 541 14.00017 7'7 535 b37 54o b I S . 545 547 550 14.000 17 191 3 35? 552 13it' 5.i 255 3 54

g:% g5 g59L 4L

ell I Of 16. 0,1 w~' 0I. ~~L)&I~IJ*S~. j 1 i 119 0 2 3/ V9 Iu " (*"

: 3 I It 1.) 90 1 11 01th . y,

e.* I 6 1 29 .1 / '~ ri . J:R394 'i' 96 I6.00

41 of H 1o0 102 lub I 1 I2 148 161 190 16.09634 54F 51 18 '47 210 -A 11 335 35. 381 41 8A 462 49 1. e *09034

946 61 511 521 564 53l 9b Vt. 97 91J 100 103 16.U9 63 71 137 11- 127 149 169 193 220 249 2I3 314 16.)634

r-,.6 Al 339 .359 3866 423 461 51) 516 534 562 580 16.; 9634 f-,4 l 9I 96 91 I 100 10: 1 108 11b 12 9 [So 16.u9634

f, 101 170 195 20 25a I 341 361 .3 A8 4.26 16.1)9b34 6.946 4 41t 504 519 537 562 S.L 100 103 10Hn 116 16.09634

6 46 1?1 131 151 172 19t 221 bi 2. ?? 30 345 365 16.q9634 111 4312 Lt Ll SU4 524 S41 562 t0i k 328 350 16.o9634

A Q 141 309' 396 433 4t30 1 529 516 564 .580 356 16.09634 -: 151 37'.. 399 45 484 520 bo bb . 81 360 16.09o34 4L 6 161 40. . 43P. 4h 1 526 541 bsbt o 5-H2 405 439 16.09634

6946 171 4.-I 53S SB.* 560 572 53 5 500 567 516 16.09634 5946 181 San 570 572 575 b.9u Sht, .5/ S60 582 .585 16.09634

-916 191 5883 587 Sfi7 bb7 548 bb* 591 :9t . .95 95

96 1s 111 120 115 11) 1 e2 134 144 155 1134 16.0498

11 172 119 188 200 216 L 1.1 3170 100 102 16.U9898

lob 113 123 132 144 1-I 18 199 222 242 1;).0Li988

. 31 259 273 291 317 348 3 .3/"139i 394 95 90 16.098V8

6;60 41 91 98 100 1 107 11 125 1'i8 168 190 16..0989

6960 51 21d 247 261 311 335 355 3;12 419 463 495 16.09d98

69A0 61 511 527 564 Sill 95 97 98 100 103 16.09u98 71 101 115 1e8 149 169 123 20. 250 2?a 315 16.0989d

6 A1 339 3b9 38r t 24 .68 4ul 51 534 562 560 16.09891

9! 95 96 91 98 100 103 108 116 1?9 150 16.0W9.

6 101 17i 195 21 251 2S J1) 34J 361 369 4?- 16.09896

f-96.I 111 411 5O4 519 5.7 562 b0t 101 103 108 117 16.09898

:050 121 131 ' 131 1/2 197 222 28i6 321 345 365 16.09h98

f 131 392 430 475 Sub 524 t)4. 55 560 328 3t0 16.09896

141 3/o 396 43% 4M0 514 529 546 bu4 580 357 16.09P.98

95 151 3 7 400 436 44 5 0 - . L6 5,1 93 0 . 98 59 0 161 403 43A 487 526 541 S69 5 406 439 16.09898

p ;6 171 419 36 S 560 F1 2 wI btS tu 567 57b 16.09898

A6.960 181 slii b70 ;72 S5u 4106 SP) bb(J 5a2 5 5 16.09898

P. 90) 191) 586 587 by,7 Sb d3n 5m b0 5v) 95 9b

g aw.

13 1i IJ 1 . 3 1 Z h.9. 1. 4 ~~~~ ii § 4 -9 /0 o I ' " J 2 > i 9.9 f' 19 ~31

1 ~ 36 1 4b1 1l . t, ? I " ) . S0U 1114 614 L-2 4 0

4 21q 2./ 1 ?o 1 2 b0 i9.?0U04 I 9 6 96 91t 113~ t 1) 95i 9$

-9 190 10 109 Il 103 54 I() 12 .* 12 7- 1 01 9 O 1 2 19 200 04 H i1 3 2 49 1 0 (To 160 /31 0

1) j L t 109 11~ ka I4 i'.t9 4 17(-, 1962 0 1 i 19 20004 2Oj5 f Li11 23 0; ?'~ n:/ ?-.l I6 8 193 201 19 -2 0 04 20. ?-i Po 2?- 245 s265 ?6811920001 J ( ~ 2 0 2 64 1 99 o1 1 9 . 2 o t . 1'3~ 4 il 2 1 e~ 7 100i 264 2 219 2 1 , 19.2U004 1 3 4 ~ i273 2 7 P1 . 73. 7 2(76- 2 8 2 ,10 2 7719110 103154 .191 274 ./ 220 6i 2"1 190 -7 2'J '30$

1 U 2 L2 7 f 1m 1 0 9L 0i 2 71 6 -.b1 01 7B 41 21 9 1 9 . L 0 4$

I~~~~~ "31 137 1644 169 0/ 19 ) 1 2 215 i92 L 6

11 64 l6 ,) 1 1 11ti I o 13i (9. u 6 1 ~ I .3 ~ 1 6 11 vi2 ~ 2 4 ? 3 2 1 1 02 5 9 . 2 0 10 lot 113 1 ?-8 )

I9 99j 98 14199 1 19. 1,-) 6 703 10 . 1 l161 1' U(1 1 1)4 1. 1 () 1 o2 1 7 18 12 (0 1 di~ Ys~ iu hS 7 259 652b 19. ui . 25m 7.,99

9 .? fj t 1o 999899 19?U -1 1913 o3 ?di e! ,'u b19t9 216 '2e9 J.u 1~ 102 1114

. 6 1Al 100 103 19 ;j 015 6 .% 13 1 1 ,1 1902j 4d i s ~ 6 932 1 . 0 5 Y 200~ .:AY

19 O ... 6~ 5 *?4 68 19 20 11 15

e~~~ ~ *.6.. SLI r n Y!~ 241 2* ?4 r.? ?6a ?"0 ??1 19 2315c 19ii j. ( ;14 27? 2 3 /j2' 427 6io2'/? 19.?0156 1 3" v 21 72~ fdt ?i4 /! 14' ?8 1'9 01

q -ti1 8

SECTION III

STRESS COMPUTATIONS

Thi section deals with the actual s'tress computations and comparison

to allowables. The stress calculations are performed by first justifying

the nozzle for pressure conditions. This was done on Paget-7. Secondly,

a combination.of stress indices from B31.7 and various other literature

were obtained and moment loading is defined. Thus, giving the several in-

tensities which is associated with applied loads., i.e. dead weight, earthquake,

and thermal expansion. Thirdly, the bulk of this section deals with the calcu

lation of thermal stresses.

The thermal stress calculations are performed using B&W Computer Programs

91206 and 91032. Program 91206 uses the virtual work method to solve axisym

metric shells of revolution (See model on Page3-1). Program 91032 is a general

thermal motion and stress program solving for various shapes using appropriate

classical theory. The portion which is used in this analysis is the opening

in a cylinder using flat plate theory modified to account for curvature in the

circumferential direction.

The stresses were generated by inputting appropriate temperatures and geo

metry into the programs assuming no reactions at the nozzle to shell intersection.

A two element discontinuity analysis was then performed and forces and moments

generated were then superimposed, on the thermal stresses to give a total thermal

stress picture.

Stress concentration factors are obtained by using indices of B31.7 and other

sources, and finally a fatigue analysis is performed of the branch.

I0,

0

- $ K

4, 1o

- 21

27

~27

31

.3 Z

SUE::CT 6uiS 12co RA~~tALj SC. ATE

Allo0..fitW D^ YEA'j rAQlUS. .8...2_.COORDINAJE_____2_.000 **.*___

SEGMENTAL GrE1Et 14lA bY GkOUPS

SEGuErNT DATA CENTER OF CUVATUNF DATA 60 1 *....* 4** L ! --. haUtuS - -. Z....__ ftRVALIPF

Str.G PAO. V-'MIUS Coumn.. TO CLNTVR COOkI. IDENTIFIER

. l.II 115.00u -U.60 -0.000 -0.0

7.0 1.1 14. Ju -0.000 -0.000 -0.0

J4.0 1 2 1 . to 130 - 7-0 0 I)- 000 -7

.1.31n 13.?5'0 -U.uG -0.000 -0.0 11---.1613.00 .000 uc-7.E (Guo .-4) 0

14.1 1.3it 10.712 -b . U0 -0.0o -0.0 i:.3 1.31A .C.'0 - 0. 000F-u.000 -o0..0

1.37S- -10.100 -0.O00 -0.000 -o.0 17'.4 .37 I0 ,0 -0L00 . L - -0.A

S )1.0 1.: 10.260 -0.000 -0.000 -0.0 .,t 1.17, *9 000 -0.000. -0 0

21.0 1.375 9.o,2 -0.O0 -0.000 0.0 2. __6.6..r J -0.000 _-0.UOO ..-0.0 .

e3 . 0 1.4t9 -*Ou U. 000 -0.u00 -0.0.

k4.0 -. 9A.S 0.00 Do-0.000 -0. 0 7-0.

th ,~o 7.5,*4 -U.000 -0.000 .- 0.0

<0.0~ .. r:071 u00-no.0 oo -py 050.0 2.184 4.314 -0.000 -0.CO -0.0

33 0 .-.. . .

... -79 . -.-

0. .- . .. . . .

47

----------- --- ------------ ---- _ -. -.-- - -.

SEGHENTAL uEONETRY 8Y SEGMENIS I K= SEGMENT NO.

M414RADIhJS K41-RK5 --. K6 -- K7 _RK8 ___K R(K-1L() ..W. ..('.)RI.)______________________

1 1.2 1.2 1.2 1.e4 1.28 1.2d 1.2d .28 1.28 1.30

___ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ . 1 __ . _ _ .3 __l3 __ . .3 1.32 _-- 1,3d -... .3 1.38 1 I. 3 S. _ _ __ _ _ _ __ _ _

21 1.'d 1.38 1.47 1.47 1.47 1.47 1*4'1 1.65 1.83 2.01

3L 2.. 19 2. 19-- -2. 19 2. 19- - ---

7 r0OHDN E.-- ..-.--- -.- - - - - . . .

O ZI EI) (K) Z(K*I) Z(K*2) ZIi(3) Z(K*4) Z(K 51 Z (r.*6) L(K*71) Z(IK*

1 I 3.2i 13.00 12.24 11.47 10.71 10.50 10.50 10.46 10.26 9.78i

.29-.. *C6-.9o*06...9 .. ....... 5S- 7. 5.72.....5e - .Z *72 - 1-__

31 4.31 3.21 2.10 1.00

--- _____----- - ---- --. - - . .- - - -------------

'4b

TCP OTTiM jP THICK, VOLOM1 HICK,_________________

5U. NO. SFG. NO. OF IOP S G. OF bIlUM SEG. 1.00 5.0 . .36 6.C3 4.00 .44 .4 '.00 10.00 ,__ _ _ __44 _7

1A.0O -0.00 -0.00 17.0 21.00 .75

1?.00 ??.00 -0.00 -0.00 . 26.00 .5h

__ 1..00__. 30.J .00 .5 .. U _ _ _ _____ .__ _ __-_ _ _ _ _ _ _ _ _ _ _ _____

31.00 33.00 2.00 2.00

.'ENTAL THJCKN!ESb hY SEGmENTS

TnICKNESS At TO OF bEbMEiiT (hA) K HA O) HA (K *I ._4A(K.*2) AJK.3) (K*LMA.5S tA (. MLA(.7) .. MAIK*8) HA(K*9)

1 .31 .. in .3A jh .38 .44 .44 .44 .44 . *65

II1a . - 0 7-- - 1 * 7 *-.01 .. 0 1 - 0.0')0 - o 7!5 .. -7.7 5 .. 75 21 .73 (.00 .56 .!b .b .56 .56 .92 1.28 1.64

31 -?),0 -240- - -. 00

IC1: f* ESS AT .IOT100 OF.- t."F I r ( .

K H.4M(sr) HEl(K.I I H *(K#2) nd .3) (K*3)) (8(K*5) Sd(K*6) hB(A7) HSB(-K8) H8(K*9) 1 .3-____.i'I __.3P .3 .4 .44 .44 .44 __.6S __ .87 11 .37 .7 .m7 .7 .87 0.00 .7! .15 .75 .75

I .7- - o.b o *5 ^ . *. .13 . 6__ 0 , G 0_ __._2 . 0_ 31 2.00 2.00 2.00

---- ---- --- ---- --- ---- -----m- ----e-

. *

.. A ~rl~ IUN16.

........ FLEXIBILITY- HATRIX.0OF-ASSEMULY.AS.IN PROGRAM 900.... ~(THIS MATRIX ONLY IS ON A PER HAIJN BASIS)

.-. Qtl N N)Q IN) ________

---... OTATIONO(0 3.138385E-06_. 8.O'1SIl7E-07.-4.?6os3E.19 .14O2074E-1a . .. . DEFLECTIONIO') '8.041817E-07 S.06477E-!O? 7l.,8k?ac-20 6.530333E-19 ROTATION(N) ___.= 76O3l9-7.6b22i!8E.2-4. I37 25PE OS. m476880&-08_----.-*DEFLECTIONIN) 1.402074E-la 6*53aa334.-19 i!..7688OE-08 5*410d59E-08

NQTJLTNE.1*I SIGN. CONVENT ION-IS .USED.iN.THE MATHIX PiRIrjI:o. HERE.- -.

* IF IT IS OESIRE0) TO USE ThlE -1 SIGN CONVENTION~ TliEt., THlE S IONS. AHUSJ. -E.CHANGED.0N .ALL.OLJKiEOVL-tD1AGONAL -lEEN.TS - - ---

- - - - - --7

-7 7 OSC 152 2

33 9 23

3 -3 -d

. 1 1o 1. 1z 1o 3 o

i -5

-3 3I35e3

1 17 _ _o _ _tj

3 3 rs 3&95 .3

lyf~17 f7 1 53 o tyu3 -- T

JoL SC A.4.c (O S "7 8Y --.'. aii . S L /o - = ": -

----- ~~#"14 I-- .l . .!J .. -- - .-.. PAGE 14.

INCIPLE ANALYSIS

.. .. ..rr-- - - o.?? . ** .

OEUGMEK TIE2 _-T -) . INSIDE UTSIL-E -.TSIDE 4. S_.SEGMENxj TI. .T2. 2 72 27 .27 27 17 T3 .T4- . TS 27 -.27 27 27 27 17 0 77 77 *76 75 2 2 27 27 27 27 . 19 ..120 115 112 1

5 .2 27 27 27 27 19 31 12 - 125 122 120 2 7 .2 7_ 2 _ 143 _ 13? - 135- - 3 130 -__ _ _ __ _ _ __ _ _

5 27 27 27 2 7 2 1 21 15)150 * 5 .3. ISO ISO

-_ 6__ .2 7_ 27_ -22 2 4 11.5 142 14N6

. - 2 2 9 - I............22b 0 150 150 150 7 28 24. 2 8 8 2 1) I50 I .o 14i 15

- . ~ ~ b - Ib.....)__ IhI ___16 0__________ 0 33 33 . 32 31 31 25 19 14 193 1 .. 160 110__ _ _ 36 38 3 53 4 3 6 . 1J 211 - 210-~ 207 - .205

13 . 3_49 _ 8 .. 646... 45- 44 .28 7! 242 241 238 236 1 *77 6 .5 S 2 2 9- _ .7(. _ _. 2 74 _ 2 72 ..- 2 6 9 2 6 7_

13 59 57 56 3 0 3 0 305 304 301 229 9Oil 14. 370 9. 3 873 3 332 893 156ao s 6ST 2.- -. 0- _31 37( - 7777777j. 3 0 3S 8-1 0. 77 1S 10 -8 31. -38

40;7 - - 2 - 5 3 399. - 392 . 430 420 . 415 410

-----------**--.--

. . r 0 0 6 I 3 3 I -. -'. TEJ1_PAGE17

-.... PEAK FORCES AND MOTIONS

POSITIV9 aA..ECjjqks .I. A4E-45FOLLOwS--

_____ TOP OF. SEGMENT..NO.1 SOTTOMpLHAININGMN S . RA0IAL------- TO THE LEFT RADIAL------- TO THE RIGHT ROTATIONAL~- CLOCKWISE ROTATIONAL~- COUNTERCLOCKWISE

_A X I A L _* * * * D O W N W A R_

-.-. SIGN CONVENJIGNS.ARE.FOP A RIGhTHAND VIEW **

&EG. LOC* . RADIAL HOMENT AXALOC TTIOAIL FOCE A RADIAL NOTATION AXIAL ... N.. OTION _MTO

____I __TOP __0. --2.9212E-03_ 0~______TP -.Ae-

_

1 TOP 7.4229E-03 -8.8319E-03 .Ot TOP 3.A3E-04 4.6174E-24 0. 2 OT.* .2215E-01 -8.6229E-03 0.0T. 3.1831E-0' S.7149E-09 2*4844E-04 3 OT* 2.396E*0 -I1.7722dE-01 0. .S0 T 3-.-101E .- 3.5021E-08 4*9688-04 3 *OT. 2.3696E-60 -4.7ddE-01 0. 60t.- 3.18144E-0-, 6.4591E-08 7.453)E-04 bTo. -. 3d80E*02 5.6-4*43d d _E*01 0.* 8OT..3.1767E-i4 -*2.34?LE-06 9.9375E-04 o bt. -. 2178*02 5.63d*E*01 0. 60t. 3.157JE*-U-* 1.2573E-05 1.2429E-03

7 OT. -1.5387E*02 l.240ZE*b2 0 * 3.1912E-0G. .. 300-05 1.3072E-03 S60T* 2.1354*02 1 3.9537h-GS 1.3087E-03 *T -6.6127E*032 -.588E~b2 0* 80* 3.6tE-04 _.5.2172E-05 1.401E-03 . T* .-9.09i7E*02 8. 51SI E*02 0 . 8T. Z3.9F-u' 1.764E-0S 1.7341E-03 I BUT* *8.41 JSE*02 lullE*03 0.- ij 4.2136E-ut*. .1.106E.-04 1.877E-03 2 O.*_l.7556 &E*03 2.013E*03 0. 80* .5 uE-04 -.16263E-04 _2.1160E-03 3 1.% *2.6600E*03 4.086E*03 0* OT. 6.36SadE-04 1.7263E-04 2*4,JlE-03 4 o*U 4.7045L 03 4 .? 6JIE*03 0 . U T. .S503E-04 4 2263E-04 -2.983 -03 _ _ _ 5a807* 9.1787E*03 2.7/27E*03 0* 80T. .O*SO3E-03 4.4408E-04 3.032.E-03 6 60T*.. 9*17876*3 2.7727E*03 0. 1.066VE-03 4.080 332E3

6 SOT. 9.177E*03 2.7727Ej03 0. bO T. _100L-03 4.440AE-04 3*O060E-03 I GT.*. 9.776*D3 2.3JLL*02 0. noT, I133'.E-03 4.513E-04 3.0333E-03 3 6CT. - .291E*03 3.534CE*03 0.* . - 80,.I.256E-03._ 4.5547E-04 3.2142E-03 iT. 2.I96E*03 *2.*27E*0 3 0. DOT. 1.49ceE-03 3.0934E-04 3*766L-03 1 BO*. _-3.765E*D3 -. 1127E*03 . 80 SOT., 1.591 IE-03. I 1.1027E-04 4 .3 551E-03 I SO .. -7 .74d9E*0C -8.5530L*02 0. ot* 1.S861E-03 4.39:0E-05 4.6787F-03 bOT * 7. 7 j26 vE* 01 -78.0b23OE*02e 0 . 80 1-I.67tE1-0 3 -4.396 3E-05 - *.6746E-0 3. _

I SOT e 7.426.*01 -7.325E*03 0. 8C* 1.672biE-C3 3.6975E-05 4.6928E-03 B .-- 1OT* . .931*01 I.327E*03 0. SOT. 1.6444E-0.3 6.437E-05S.1687E-0380. 2 . 9337E03 1.36'7E*03 0. -* 1.bl4U0-03 3.3124E-0 4 6.290'bL-03 80T* -I.2901E*03 I.936E *03 0 OT- 1.*9913- 0 3 4.7541E-C4 6. 9 03 3 E-0.- BO. -. 63OE*03 3.7E*03 0. 8OT. 2.626bE-C3 S.8482E-04 7.85bE-03

_ _ O T . -_ _ .I 3 3 9 E * O 2 . 7 7 8 4 E 0 3 0 . , - . 3 5 0 0 E - - 5 . 9 8 . . 9 5 4 9 E - 0 3 80T. 4.8234E*03 '.1337E*03 0. * 80? 4.354E-3 5.767E-04--8.9549E-03 --~4.37E0 0o. t... -*. 11-3 570E0 1.02085-02.

0 0 61 3 3 * -.- I~~~.. I'LHA 1 N -48169- .--. PAGE.. I a-. 30- aOT*--..3.sagsE. 0 3_ 2-2aISE03-o. -. BOT.....4 91 E3- 541 G6E-0.___I634.E-O2-_______--~31 SOT- -1.4S49E*03 3.6190E#03 0. 80!. 5.5010E-.03 4.u9-o '.9-0

33 OJ - . 0.-0 GO~T. 6-3E63- 3 2.6999E-G4 2o346E-o2 (FORCE AND MOTION OUTPUT IS IN GLOBAL OII ECTfOM;' R AND Z)

- ----------------

OSC 1522

7i~ 4 -lei

Jo oo .

1, 11

3k 13 Ilq Itt

12

24 Z ,

.1 2

33 3- o 343

13 30

I J I_3___37

aZ2.

o4a 3 1712 17(a

.: We 'Is I___So _I_2

MrI JOS No.

Zu-J-r:T /7 "To Sc 4L0 ________"T

' - IT if . t ( L. .. t t *1 /. *'., -- ' 15

,* I . G L. /s_.'._**_.._ I flAYE 1

TETPERATUkES PER SEGMENT USED IN PEAK PRINCILE ANALYSIS

OUTSIDE INSpDE OUiS DE INSIDE SEGPNJ L .T I T . . T3 . T4 .JS. GHI Ti T23 T4 TS 1 25 25 25 2S 23 17 63 60 60 59 _ 5 2 25 25 2S eS 25 -__1 a 72 71 70 68 67 3 25 25 25 25 25 19 -96 93 88 86 225 262625 25 02 195 1 1 0 139 1 525o 25 251 21 125 120 115 69? 110

60 25 .. 25 2S 25 2b 0..22 123.. .120 1159 2 11 5 0 ___ 25, 26 2!; 26 .2b 23 ..... 1a2i_ 141 115....31: _ __

B. 23 296 217 21a .126it

6S4 31 315 350 3-3 337 30

__ 6 3 6 .26 .Z4 _ .12_14114 .:

1 6 623 1670 16 0 169 . S2

27 2 7 2 7 -- -.. 2- -7- --26 - - - -. ._ i . -166 - -- 1:-6

'- 4 3' s 4 -- '

-..-- - -3:5 -. 3o.'.3 3 7 c 300 2.2150

0 00 6 I 3 4 2

S. .. TEHATfON..'J14Z1 -- PAGE 17

PEAKFORCES .AND MOTIONS.. *************** - .. .... ~.

POSITIVE. DIRECTIONS .- ) AREAS.FOLL__S_ _

_TOP ..-OF SEGMENT NO.1 ROTTOl-OF..EMAINIG.-SEGHENTS.

RAnIAL------ TO ThE LEFT..__.RADIAL------ TO (-E NlGHT. ROTATIONAL-* CLOCKWISE ROTATIONAL-. COUNTERCLOCKWISE 44A.AL****** _UPWARD

x4-.00 WARD

-IGN CONVENTIONS. ARE 0R ARIGonJ HAfD VIEJ SEG. LOC RADIAL MOMENT AXIAL NO .. FORE - EIA LOC* 01DA NOFATION AXIAL FORCE. .R

.. . .MOTION - -. .MOTION iO _ 0.0 .- -U3 6. 359E- 4 _ 0* TOP_. 2.946bE-04 . 1.65 4 4 E-24_

_ _ _ 0.. I GOT. -3.0525E-u3 -6.2260E-04 0. *OT, -*9 -u4 7.4682L-10 2.2997L-04 -U1 -SJ,!--3.525S3-02

- 2.?2brjE-OZ --. 0. 1 6 60 5".E-9 4.bg L4~ 3 b*Lj. 4.1391E-01 -1.1213E-01 0. SOT. 2.946E-34 -3.0203E-09 .89992E-04 ._BOT* -9 2 703E-01--4.382oE-01 0. 80T. .946E-04 30 -096992E-04

S B31 -1.6094E*01 9.090JE*00 0 80T....2.9454E-34--3.37SC-07 9.1990E-043 6 6T*..-1.2384E*01 .l.2911E*ol 0* DT. 2.9.5- )4 2.4AOE-G6 1.100IbL-03

7 80T. -3.9001E*O1 le7910E*01 0. 1. .*952de- 34..41137L-06 - 1.207m-03 d..0.-.80* 12.7717E*01 0 Bol* Z . 9163-,1- )4 6.49560-06 1.2657L-03 d.-- BOT. .. 9.hiROrE-o I 27717E#0' -0. 8Ot..491eii.4 .8f3.*O..O131E-3 ___________ 9 5cT. -5.037tE*0Z 1.92i3E*02 0. L0T. 2.09i-)4 .4.8.37L-0b .. 30150-03

10 0 . - 8 .7 1 2 E *C 2 6 .b/0 74r.E *D2 . * . 9 - 4 2 . I5 9 4 -05 -0 1. 538 -0 3 _ _ _ _ _ _ _ _ 11 R0T* -9.41h6E~u2* 8.31)b7E*Go2 0 32304 487(0 1.5724E-03 2 60O* -.o* 4E * 0 3 l*9Yb6E*03 0. HOT. 3.33570-04 6.2669E-05 1.6365E-03

13 80 . -2.655 4E*03 4.084E*G3 0* b0 . 3*611W-04 _._119a-04 1.8584 -03 14. BOT. _ 2.9129E*03 .4.7240E*3 0. 8O.. 4 .65s/ -* 1.88986-04 2.12e1003 i5 S* S.6E*3 37d o3 080. 614.- . 2.6402-4 *10E0 'a BOT. S.6630E*03 3.7m3aE*03 0* 80T. 7.273::-14 2.9142E-04 2.512E-03

!6 BCT._ 5.66.3E0E~3 3.l1i~aEou3 0, ouir___64 -04T-. *7 . 5.744bE*J3 3**3 ~ 0* 80. 7.50 .2. 91420-04....2*4904E03_ 1 Sl.C* S.442E*G3 2.31.0E.03 0 * 7*497L-14 3.051.6E-04 2.5179L-03

60.SO* 4.12i5E*03 -1*9H11E*02 0* 601BO. 1.062dVE-(4. 3.5753I-04 2.6939(E-03 BCT._ -1.1c02E*03 _-1l33J3E03 0*. O.BO* .2367.-C3 3.261 0-04 2.99OE-03 1 DOT. -S.6'"43E.03 - 3 .14"3E*G2i 0. DOT, .237?:-C3. 1.2S4,E-04 3.7 4E-03 '2 - OT. .- 5.69 3E* 03 -3.14 -i '1 2 0. DOT* 1.23740-C3 I*S544E-04 3.7; -L-03 3 .0. -5.3533E*03 -2.013j5 E*o2 0. BOT *. I.335 .- C 3 .1.S.4E-4 3.70 0E-4 : O 03 oOT. -3.1249E02 9.7231E*02 0. DOT, 1.3 321-C3 1.4947E-C0. _7.dCE-03 Z 3T. -4.47E*0. 9 .39'feLC2 0 - BuOT. 1.,711.-C3 3 .0177E-C4 .110E-03 a- 901* 1.i07E*03 1.4871E*03 0. DOT. ___I .730L-03 3. 0 7 44-04 562bE-.03 7 S0T. *S.3764E*03" 4.4528E*03 0: . .34-0 .7 - .. S.6bE0 7 0*. 7.021E04D0. OT. 2.2741E-03 S.4323E-04 6*485E-O3 e3T. -7.6*I1E*03 ._1.22E04 0. . OT. Z.918U.-03 6.1452E-04 7*.4b4!E.-:-03 ------ 6. 1 E.0 . 73w 0.. . 3.64.'E 83.4647E -04 8.5706E-03

(A ----

6 O69~ 34 3

GOT. -Z. J544E*0.Z __2.3130E*04 .? BOY. t_.4350E-03_ 6*4504E-04 987E-O3-03 'COT. -6.7521E*O3 2.0795E#04. 0. 801. S.1584E-03 *6.k9O6E-04 1.2237E-02 GOT: 1.3098E.04 -9 .8460f-.03l 0.--- a80t.- .613E-0.3-.5.48S')E-OQA . 5024E-02_____

BEoY. -0 --0. lJOt. 6.416 4E-03 '3*9259E-O4 1*8195E-02

-- (FOR~CE AND MOTION OUTPUT IS IN GLOBAL 01!tECTIONS A ANL) Z)

L4J

0 SC 1522

1

I24 5/ 7 45

If

.7.

I ig st I -- 1-0

3 o

t o I 4

110 1 9i 7 5' I

jz ~4 7'~-. __5_7_.

: -. 7 :- 37S .. .__ _

-in - - .

r. ... " o.t...

w u -- -

ooo6I~e 4 a

TEMPERATUR SER SEGMEN USED IN PEAK PR CIPL ANALYSIS

OUTSfDEINIDEO SW SE ET ir INSIDE OUTSIE INS E

_ _ T 5 T 2- -_ _NT 3 J 4. S o M f rN_ T i _ T .-. _3 _ T 4 . __, 2 25 2S . 25 53 60 60 4 So Sd 3 25 25 25 25 - 25 .0 _ 6 67 3 25 25 2 525 25 19 93 91 90 a6 7 4 25 25 . 25. 25- I2001. I

25 25 .25 25 25 21 -117 115 112 110 6 2 __ 2S....?5.2 25._.. 2S. -. 22.. .20 -_ 11I7. Its~.. . * .. . . 7 25 25 25 25 25 23 20 117 - 5 112 110

9. 226 26 26 26 25 65 184 163 162 1.30 I 2 _ 27 27 ?7. 2.- -'26 28 . 179.-... 17- . 176 175 12 28 28 25 26 .28 27 :'io 2L~ 60 2t5

35 35 3:. 32 30 2- -q-_ 236 2 _________ 43 5 3 9 - 3 6- 3 3 - -2 9- 2.... ..... ._ 23 ..a . 13 .--0 45 43 39 36- 33 -70 269 68 26 26 1 6- 60 54 _ 50. . 35 3.00_0299. 298 26 295 - .a.- 16 63 60 65 so .5 31' 3 33-9 336 331 327 . ~--50 32 3 .. 67 - -.. 3 80 .-.. 3 7 3 -.. 3 65 - -3 5a - -33 '30 420 410 400 390

.......- - -- -..---------.-------

A 1ILA1IUN.:,!z659 PAGE 17....

POIIE.IEUN- ARE. AS SOLLOWS______ _______

RDA----TO THE LEFT..-_....R.ADIAL -------TO *1 IH....__ ROTATIONiAL~- CLOCKWISE . ROTATIONAL-- COUNtTERCLOCKWISE .4~IA-,. ~ t--u5 WARQLL AXIALr. .- -.- OWtIA)R0j..---___________________

*.SINCONVLNT1ONS- ARE- LOR.A.RIGhT. HAND V L~:~...... . ...

SEG. LOC. MAIA OMENT AXIAL LOC, RA(~il.L NOTATION AXIAL -.- FO.ICE - . FORCE___. Mn('N . .IN -.MOTN..... .

.1A......TO __0. -1883E-o.__ .0D. ___________ TOP -2. -04__.....6S4'E-24 .0. ______ ________ 1 801. -2.-9'hE-o-3- -7. B~DE-04 0. doll Lli4b'1-64 -7.'9j'ebE-10 2 -2-997 E-04 S2-80tno._ -- 3.5313E-oZ. 2*;!o51*.-2o*-0 54(_.UJ.. ..51Eo...9,!~~ .. . 3 30. .8'*-1 1O~E-l 0. boll 2.' 461E-04 -2.4574E.-09 6*8992E-04 7 4 0.-.PS84E-o1 _- 4.4503E-01 -0. t.- .4J-4.337E0.91c-E0 5 eOr. -1.607,SE.O1- 8.99931000 0.- .801. 2.94';,1F -04 2.4372E-06 1. 1SuoE-(j3 _6 o _ CT.--1.26t7E-0 1 _1.2b4:JE*01 __ 0. BO. .-c0u~4- 4..015E,*o6 __ .20 15L-03 ______.*

. 7 BUT. -3.9 71 1E*01* 1 -7465E 0 1 0. BOt. L-96dE-. . 6.4412L-06~ 1*2657L-03 6-87 -9.4;924E * 0 1. -2.7H9YE 0 1-_0. 80 81-.z.970=E .7b4.o6_ 3.04-3 5C -5.0762E*02 .1.9'.06E*02 0. .801. 3 -051"V -04 2.467'iE-05 '1.'.35fE-03 10_ bUt. _ -8.7h521.0? -b12'E0 _0_ 0.-4t .a..3z.E..4.b44.o ...7TE-o3---.11 51 955d.Z 84312E*O;! 0.- Sol, 3.335SFE-04 6.3047E-05 1.6366E-03 12-80T.- -I.98oSE*03 _2.o016E*o3 __ 0. - 60 - 3'82t E04.1 12E0. -- I *8564E-o3 ________

I-- 80tr.- 3. 1773E*o3 4.b5,14 -o3 .0. -___ b80I..__ 6 e53- 1 E-04. -. 2. 7r.OOE-04 -..2. '1LW-oa*. - .. .

l!) 80i. 5.4471E-03 3.Seo9E-03 !*0. HOT . 7.2j'11E-04 Z.808?E-0. 2.5117iE-03 1CD 0I 5.,-7 If ,13 .3 .5____ 2.-4 7z 3E' 2.3 -- ~ ~ *2'-;E-u03___ It -0' .C.:t*3 3*3.Z"je. 0. *~l 7. 7; -5 2 *037-6E -04 2.51'1-'--C3 1-. 10. .1471IE.03 2.C'11)IE*O3 0 0 . 601. Iv d I- 04 ....3392SE-04 .... 6sEO 11 0bO. 4.235 1E,.03 1-6. Ib,'UE* O 0. 1.101. 1.07iu;:-03 3*2947E-O'. 2.99lbE-03 20 Bol E -O.*)42c5E*3 .- 1.5214E-03 0. .8_____101.. I .214Ui:i 03-20c)3E-0/* 3.'%~E-03___________ 22 hOt. -6.17'.7E*03 -6.20.EJ~ .. 0. ' 0._ .0)13 .4 -04 E_369,.-03 ~ ~ . ~. 23 HOT. -.3:.3-S*03j4E04 0Q bo1. I31Jd;7-o3 1.4784'L-0. 3*711';E-o3 . 24'. B01. -7.37:,E*0Z ._ 9.OII4E*.2 06 60F1. .334:1-:-03__1.22IIE-0. '0891E-03_____________

.2b POT. ..- 1.4772E-03 I *73Oi*03 __ 0. br .7J-0 .18Eo-_559E0 27 8O. 2.67E~3 .SaS.0 o OT. 2*22'.d1:-03 5*.4265E-04 6.3'469F--03 26-807. -1 .9796E-03 S__.9797E.03__0- 8 4-I :3 58679E-04 7.as842.-03 24 a0r. 4.7655E.027 7.902E03 0 SOT. 3.59.'-1:-03. 5.0',942E-0c. S-3628&E~03

0 0 0 u'' 5 4

6OT. 2.0307E*03 8.7653E*03 0 HOT. 1.1882E*03 9.10S3E*03 . 80T. S.022E-03 5.956E-04 1.98E-02 SCT. _6.8736E*o3 S*5491E.*03 0* BOT. S.64 -03 5.7961E-04 1I.466E-02 607O. -0. -0. -0. HOT. b.642.03 4.9681E-0 1.7663E-02 bo* 807T. 6.12tOE-03 3.19E0 176 E3E- 02

(FORCE AND MOTION OUTPUT IS IN GLOBAL DIkECTIUNS R AND 2)

-

--..-...--.

S*- -. ..

OSC 1522

o 71

7 3 71 7:5

- - 7 7 9

7 o 'jI/4'_ 15~

1J0 Ig, I/3 5 55z I w

71t . 1. .-.

3*5 So f 1 3

2z 3 ) I 4 4

S .3s 341 -S1 37 '7Z

S3U 39 swl 403 qoj

_ _ 9 4 2 ' j 3 .7 e o q < 2

OI I 196 1 4 ' 35I( ta

IAt

-6r1 6 o .s.

.- . or et.0L :. <0 ~. * py

.. ... . r - .- .- .- -" a c

0 0 06 9ob 34 9

TEPRTRSPRSGEYUE NPA PkItJC19LI. A-NALYSIS.

O U TS I o r.---- - .. .

N T I T2INSIDE OuSI INSIDE 0 -. G . . .T2 TT3 INSI 2 0 0 .0 0 0 17 30 30 30 30 0 0 0 0 o......0 1s 45.._ _ 4 - 42.... . . 40

3 0 0 0 0 0 19 70 66 64 62 60 - 00 - - -- 8 9 8 7 .b 36 0 5-. O 0. 0 0 32 9b 5 9,5 9

15 91 286

7 0 0 . 0 0 0 23 03 97 95 9 95 9 .0 0 0 0 0 25 145 144 143 - 142 142 0 . .0 0-.O . 2 6 ... . . 1641 3.. 16 142.....l Al 0 0 0 0 .27 195 191 W0 1b3 1ao

1 2 8 _ 7 -. . 6 _ .. S_ _ .4 _ 26 28.2 6 218..* 211... 2104, . 198 13- - 17 - 15

7 2 10 1?Zi C 24S ?5 225 216 _30 a 21321 11

-- -- 27-Z5.- 3 _03 _ 3_3 1 3 335 320 308 295 2d,3

33 -#30 417 40S 392 380

------------------

- -- -- - -----------

-----

.... .... ...... . . . . . . . . . . . . . . . . . . . . . .*

-------- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - --

________________J UJRAJ DLTItia:kO____ _k60 _ ____PAG-1 7... ..

TOP OF'_SEGMENT NO.1 BOTTOM fJE4" .INIGL~iET ___

RAOIAL -------TO THE LEFT _AOL-------10 THE RIGHT - .~..*_____ ROTATIONAL-- CLOCKWISE ROTATIONAL-- COUNTERCLOCKWISE ___________ A*IAL ------ UPWARD. AXIAL= ------- ~ -- _________________

-~ **SIGN CONVENjIJONS .AREf GItANvIW **.~.______. . .*-

rEG.'LO'c . il RAA Z'OMENT AXIAL LCRAILROTATIONAIL

1 0TOP - 0.tI8231E-03 0.TOP. . 4.S554E-I.....3.307E-2......09. -_ ______________

3 UOT. -7.5671E-01 3.634.2E-01 0. NO0T, -I.'.331LT-08 S.481E-08 4.2869L-09 4 ' 0STO___ 5.8706E**00 -Ij.obi3E*00 __0H______Ot. -_ 3o3'55bi-07.... Z.202bL-01 __-2.52.9F-08 ______________ __

5 bT. 7.67 3E-01 -8.5JJ'.I:.oo 0. ___OT__ 0. '-1.525eL-06 -6.05 93E-06 65.93DEL-08 ___

0I .b3T. -3.bl69L0 _8.5J3d000 0. db0-Jaui6E-06 .

PO -o049L*2 .510-0 0 01. -. ~il 0 -7.3474E1-06 3.4.502E-07 zi HOT. _-1.64OOE-02 2.06~04E#01 .0. 8(01. -7.50701-06 _:--5.31941E-06 .6.052isE-0 7.___________

' P20.- -S.42dE.02 2.20:JIE*02- 0 BO. -.16 0 .26'26L-iuS 2.245'tL-Oc6 a BUT. -9.3325E.02 6.63-o7F*02 -0. -HOT -- 3.94611 -06 -..3o9ZtIIL-05..3. H1195L-06 ____

C- eOT. -13-.730UE-02 8.9713E*02 0. 1301. 4.01801-06 5.4004.E-05 4.4731E-o6 2 __ OT. -1.52'oE*03 1.7103E*03 -- 0. _______ or. __ .05211-cs _ .O6513E-04-_ 3.0592E-05 ________-.

3 60 1 . -2.1-6I17 C, 3 3o5'0;-E-03 00 801. 1*3SbUI.-04 i.8730E-04 lo0325[-0. 1130. 2.6i!3CiL. 3~790130. 1a3 ei:- C4 -2.'i319E-U4. _2.10 74t.-04 _ _ _ _ . - -

5 HT o3G*3 3.5191E*03 0. 0i01* 3.990UL-C4 3.2771E-04 2.*i438E-O4 6 -BOT. 496130E.*0 3o7VlE*o3 0. SBJ t. 4A155d4:-C4 -- _3.27 1 E-04. _ 2.34813E-04 _______________

eaST. 4.a3Ol'E*03 3.340%oE#o3 0. HOT. 4.J?25l.-C4 3.4,266E-04 2.4593E-04 0~ 80o. S41601(03 -I.187.E*O3 00 001. ...._bo2'.d1:-C4 ._3.9650E-04---..3. 1338E-04._______

9 SO. 4.601E03 1.184E*DI 00HOT 7 o6 g1 l:s '04 3.9933E-04 5.5i422E-04 * 3 801. _ -3.S2dlE*O2 -1.24tt5E- ' 3 __0.. 0__ _ eT.-.. 9. 4 3 A1: -C4 -. 2.795CE-'. __ 8.9748RE-04____

I e EC,1. -4-5%-23E-03 -6.7' 4E*OZ 0. . U30. __.0.1-3_.2.121lE-O4...1077iE--o3______

3 S3T. -'.3e~lE-03 -5o90ob'd.2 0. HOT1. I.OS5ur.-U3 2.072GE-04 I.C99:IE-03 SOT. -- 6.3a67E*02 __ 5.2AbIE.02 _ 0.LO 801.l 1. I11 1-03.....*.I7112E-04_..1 .134.E-03 ____________ ___

BOT. -6.Z'.a'3E-02 6.9t9o7E*02 .0. O. 1 .301. i311:-03 2.5593E-04 2.2097E-03 6 OT. -3.4'a.SE -03 1 .57014*03 -0. sot. .4197V03

I BT.-1143E-4 .226E03 0 OT. 0 .8730E-03 5.3111)E-04. 3.431,0;-03 3 __BOO.-71.8ablE.O. __1.97ZIE*04 0. BOT......24367E-3.._64437E-04-..4.do3l-03._____

SOT. -1.8908E*04 3o7102E*0 0. S OT. 3.09 viZ-03 6.9348E-04 52310

LUJ

VOT 80. .6633E.04 .O*.kE*04 0. HOT, .6uC9O-3 .2G39L-L10 ;o..2 .

33~ 60T. -0. -0. -0. H01. b.a2-.a:-03 3 1.3a3:SE-oz

(FORCE AND MOTION OUTPUT IS IN GLOBAL OI ECTIONS R~ ANt) 2)

0 SC 1522 q7- 7.

I 1o i 1

01 17 03 103

0 0 11

. I1 11

I o 141

1j 7/ ITZ

ol 113 115. 0

Ln. .s .- .

131. 1A33q, If_* .5SD

.r 341 3& 370 373 3Vo

.I *~ t39 oo "03 qo&e

a Io *39 q 937 31

.ew arIST- _ _r

t!"R JO7 =1 11W :u -.u-r '// of . - 'iV. -7 D. r

*. is .: .. p . * . ,- ( DAY'- ..

0006 14..

TEmPEAUHCS PERSEGMENT USED IN'*PEAK IP4INCj,)LE ANALYSIS.

OUTSIDE S E G I NT-__-- - -- E GM U 3 TI IN S ID.

2 26 26 26 17 73 70 67 65 65 26 26 26 26 19 83 2 8 26 26 26 26 26 19 107 104 102 99 12 ______ _ 26 2 _ ~ 2 6 2 6 _ 26 - 20_ 130 .. 2 92 181 _ _ _ _ _ _ 5 2 26 26 26. 2 6 21 135- 11 17~ 12-3 120 6- 2_ * 6 . 26 ..- 26..... .... ... 2b -- ;-_ 22 __ 3 . 131.. 17 .. 232 . .... ...7 28 2a 28 28 28 23 . . 13h. 131 127. 123 .. 120 ... 3 0 ........ .. 0........3 C..... 3 0 .....

_ .11 12_7 I2_3 1_0 -- 30.-30- 30-30-2_ 15.5.153-.15115 I 30 30 .. 300 380 lo 1 0 1b0 1 O

11 33 30 32 30 31 .2 198 . 197 197 19 113.32 32 31 3! 27 ;!922d a'k s I2 2 -1 ?J43 -4 1 .-- 40 39 37 223 221 S258-253 240 245 63 60 57 54.........50 30 2 -4853 262 274 270

16 73 70 67 63 .60 31 8360 310 340 33 .65. .6 5. 30 30 32 33 .. 3 35S 445 430 420 4

-----------

- ---- ------

- - ~~ .. ~~ P E A K F O R C E S A N D M O T I O N S_

_ _ _ _ _ _ _ _

- .. POSITIVE O0IRECT!jQNS_.f 1 ARE-AS-FOLLOWS __________ _ _ _ _ _ _ _ _ _ _ _ _ _ _ T Pe _ O F .SEG M EN T NO I~ T o ~ r ~ M I 4 h S G ~ ~ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _

RADIAL-- ThE' LEfFT__.-_ RAD)IAL ------- TO IH:1 RIGHT ROTATIONAL-- CLOCKI'wSE ROTATIONAL~- COUNTURICLOCKWIS *. - . . A JAL ------- U WARQ . SEA- ---D ~ w ~ D _ __ _ _ _ _ _ _ _ _ _ _ _ _ __ _ _ _ _ _ _ _ _ _ _ _

RADIAL MtOMENT A XI AL LC RAIAL RTTO XA _1_ FORCE -FRE - MO I I ON ... - ROTATIO AOIAL ... . . ...

I. TOP __0. ..- 5.2727E-3. .TP.....306b-. _...?5E2......1 LHOT. -4.3647E-2. l366'IE-03- 0. _101. n3.064t:E-14_-I..?23E-09 Z.31-0 2 20 __ 1.1257E-02.. 8~.6ZIE-02 _0. HOT*__ _ 80 . 3.064-JE-i4 ... _ 4.36170E-ce '.E'1-4 -3 BOY. 2.2843E~oo -1.O423E*00 0.40.:OSE12 222Eo .7641E-04..

00. do" 3GSj-' 2.2025E--07 71761~iE-04 . 57 O 301. 1 .047E-01 3. 1 toE*0 0 . 003 2 7 f 0 . I ~ - S 3 3 7 L 0 8_ SOT:. t -.9 4EO ..5).4Eo 6!_ HO-'0.09 4 I 7~ .~J E8.'II.. . .16 E o 0. 80 ._ j. 1 - tC 2 21;23 -05 E.1 01 0 BOY~C. Ie-1 07i3E 0 3 __ . OS 4E*02 .. 0 . __ _ _ _ _ O . 3. o c L ..5_ 7 7 1 E oS I o 6 E-03

. 1 or -.103~~ .1.JE~3 0. HOT,~ 3.27/E-04 9.27251*-os 1./317bE-r3 8- dOT. .-4a676E . _ -514412E-00 0. SOT1 .3 1-4 14Ot-4 _19 1 E0 3 113T. -8- 13S .o3 33 ~ o - O E 0, 0OT b-..27u'. E-0 2.1133E-05 ' . 3584E-03

13-- 2~0T .- _ . m S E.0 3 3 . ) 105 4 E~ o 3 o D O T . 37 . 2n IIE -04. .34 .2 17 E- 6 5 - 5 68 UE.- 03 .. . . . .I I bOT a.103-OZ 1.1J7*03 0 OT I 11. 7o3jE-04- 3.333-0, 12.60E-03 62 LOT. -1 4.2676E -03 3.1343E-03 0. o l . 7 'E 0 93 .3533 01-7' _ l32E-0.3 _ _ _ _ _ _ 3 -E3T S 6b5 E. 3 17v',E03 . _.2 4 -636t[ 0 1.4419-04_ . 191j-03 ;3 80 . - 21E0 .8E03 0. U01. bI.2331E-o36 __ 2-3 7E;9-o0 3.64 kOT. -1.7652E.03 -1.114O1.o3 .0 . _ _ _ _ __ 1 0 . _ 3.3??2-3ao 4 E . __ 2 8 (E1 -.3

I i) ROT. 56.1O33E:.O3 291- #4 E 3 0 ._ _ __ _ __ OT. .4s7'#t ... jj ._ .33E'-04 _,. 14/f 11.. 0 3 3. 501... -S.633E*03 -1.57 bE04:03 0:1 H.O7T, 0 3 .3204E-04, 2.81 9E-032 1 . 3 . 6 4 2 1 E # 0 3O _ _ _ 1 3O b d lE .0 2 0 .*- U 1 - . -- 1 4 6 3E - 0 1 3 .3 7 1 - 0 4 2 . 9 0 ', L - 0 3 _ _ _ _ _ _ _ _ _ _ _ . .3 8 0T._ - . 368181 03 ._ _ 1.5 $381 03 0. Sol. V- .2 31 E 03 3450 '-9_"-04 _ 3.6 103E-O: .3.*. . 7 a l. - 4.733E-03. S2.83? 6E .0 "o. 80 .- 3S E 0 .20 E-o _ 3.1 E-(,3 13 0 _.8 T _ .7';-SOT._- 9.S:Eo __I38Eo 0,5 130 1 0.3A913E-04._ 1 E -0. 3 320T._ -841.04E0 2.1563E#03 . 0. DOT, 3.770-1 .51.3 13-04 4.1381E-03

eC.u. 7 3 - 2 _ .04 E 0 " 4 6 E 0 _ * 0 D -4 - -6 (E 0

30 .. *-*-*ITERATION 696 O 30 0O . -I.6053E*03 2.94'4E*04 0 . ."- ---- AGE 16 *j T 8*GS62E*03 2.7328E*0 0**5-- .. 0. . 4 -1J1-0 6.832E-34 1059

33 . -o. _O..6.71SE*04 . .3090E*04 0. U) -0 4.7736E--4 ----........ .t 036 323E-04 1.9127E-02 (FORCE c*AND )TI OUTPUT IS N GLOAL DIRECTIS RAD )

----------..--

-- a - ~ ~ *-~ -* -- - -- -- --- -- -- -- .. - ------------ -

-~ -- ---------

- ----.

- --

--------- --------

C.*

OSC 1522

17

* 107 jp' 103 0

I - v

*& z

.Z3 U-232 - 3

911 21?

L' III,

--- - - . ..-. I ''*** I* a"" - h.'PAGE 14 .

__ _PER SEGMENT USED IN PEA PRICIPLE ANALYSIS """"" ".***.:"" **4 *. ***

OU E TI INSIDE .1- _T ISiV S--- ---T 2 5 2 6 2 _ T 5 . .G 6H 1 1 .T 2 4T3 . TT S 525 2! 25 25 17 43 43 433*43 2 2 .525 2 5 2-- - -_2 5_1 8 4 _ 4 8 B _ _ _ 4 3 3 25 25 25 25 25 19 sa 58 5 - 5 - sa

?-25 _ 25 25 _ 25 25s..... 20 .6 8.. 7 3 ... 7 3 - . 73 25 25 2 25 25 21 73 73 73 73 73 25 25 25 2S 2 5 2 .~ 73 ) ... . S 773 7......... 73 0 3 3 5 5 25 25 25' 23 73 73 73 73 73 8 - .25.- .2S. L -525 -. 2S. 2- 6 . 83-o 60._ _______ 9 25 25 2 25 .2S 9 90. S 11 27 27 2 76 76. - 2 f 97- 97--- 97 .. 97 12 7 27 27 27 27 16.1 107 107 107 106 12 - ..31 - 31 - 31 - - 3 11... 1-137 .. 7.1..1167.._...1 16 11 1 3 38 3 34 34 1 2 128 127 126 12 1 5 .333...3 8 . 3 0 -... 14._ 1333 15 43 43 43 43 43 31 't7 154 153 151 150 .10 - -- .- 3 3 43.3- 437 16 6

2 ?7 - 11569 33 19,1 187 18S 182 180

* - - - - - - - - -- - - - - ~

- -

0006 35

PEAK FORCES AND MOT IONS - . . I-AI IUN j . I I - 0 .0 . 4 0

- . --... POSITIVE.DECHLUS..IREAS

FOLLObS

TOP OF SEGMENT N0.1 BOTTOM OF A 6SEG__ OTT .ROFN.A INIt.G S EWEAT

RADIAL------ TO THE LEFT RADIAL.---.- TO TE RIGHT ROTATIONAL~- CLOCKWISE ROTATIONAL -- COLN ERCLOC GS AXIAL ------- UPWARD ROAINL-CUTRLCWISE -A--........... ,AXIAL ------- Owat.AND

SIGN CONVENTONS AR .1p IGH AND.VILW **

SEGN AOC..XADIALALONEN. *- . - FORCE . O LOC* RAIAL NOTATION AXIAL F.. O C .O T I ON1 H M O T I O N TOP* *849E-03 7 .02E-04 0. TOP -2.946b5-34. -3.3087E-24 O.

0T2 . -7.0700E-0 .) E-0 2.94651:-4 -99498E-10 2.2997E-04 ~2~DT. -7O7OEO 165,E 02 0.

_____.U0 .-.1o-9- 4.b99b E-04--_ 3 ROT* -3.da75E-O2 1.62a3E-UI 0 OT. 2.946Th-34 7.6341E,08 6*699E 4 807* )T.__A4.1011E*00 .*I.7502E*00 0' ;0* d!47L47.31-8 .9 -04SHOT.* -2.6034E-01 3*I16bE000 0. OT. .2947E- 4 -3.4924E-O7 91I8E-04 o * ..- 5.5360E* 01. I.32?JE*ol . bor. . *.7-4.2CE- 1.15O0E-03 6 S01. -9.11iCE*01 3 .1703EQ1 0. --- . 1.92JiE.-.*4.23156 I.201f6-o3 S 631- -1.12,5*02 - 4.7033E*1 0. 80 * . 920IE-J4 3.0376E-06 1.2653E-036 0* -2.2:ISE.U*2 12jE-n4.__6.672tE-06

1.s2999oE-03 * 6 *..*).4311E*02 _ 2.7.TIu .E*02 0. SOT. 3.0179!-04 2*IlhbSE-US l* 2 1-03- I CT. -. 8517E*01 2.9152E.02 0.. 3.190-14 3.4593E-05 1

2__T SOT* 3*26tE-04 -3.19&bdE-O5 1.6lyE-o,3 2 80r._ -2.7930E*O2 3.6209E*02 0 80T. 3 .26 E-04. 3.9668E-0S 1.BOE0T. -7.2318E*0? 8.2201E.02 0. *1 43.6390E-04- S.844Z2E-05 1*8230L-03

1OT 1.0 0*01#3 -. 9.6.It6Euz 0. U* .3-- 9.2482E-05 S *T 2.0didE*D3 6.19*-ijE*02 0 (4 1*41161'E-04 2.306IE-03 t * SOT. 2.021E*03 6.19iE*02 0. HT. b.3-(405L-04 2.o31141 E-03 7 SOT. 2.1 3elf* 3 S.3n 7o7E*2 0. -T I*S60S -0 2.3754E-03. 6 dOT. 2.514c-9*0 3 6.Iu.dGE*1 0. 80* 5.75h7F-14 1.S829E-04 2.391£Eo3 80T* 2.0Z22E*03 -113eJ*03 0*80. * b . 4 1.6390E-04 2.474-0 3 --- 0* OT . * E* -9wSOT* 7*O64317-04 .30S/E-04 2.70oE-03

8t1* -4.0093E*03 -d.54>E.g 0. 0301* 7.074*E-04 4.30,7E05 3.1E-05 24 J 9 1 -9 ??i7E, 0 BO1. 7.b4 1i: 04* 4. 0 'E O 3 '60~E -o _ _ 1~ l13T.

NOE I -9.?0,Ec,, U.04 '..304?L-OS 80T. -6.7363E*O2_ 2.7J69E*02 0. ulT* 7.0650 -04 3.8284E-05 3 .I6GbE-03 8* 1.210E*02 3. ED2 0 -07."83e-0 8.8333E-06 33 SiE-0 3 ---

1 3 0 . 1 2 1 O i ~ o 3 a .7 , ~ o Z 0 . . h O T . U . Z o t i a L 0 4 " 5 .4 4 6 2 L -0 53 . 0 1 1 bOT. -3.2613E.o2 4.1613E*02 0. * 80 T* .2861r-04 3*4626900 .861E-03 OT* *I.4S07E*u l.312E 0OT 1.1020. .-03 1.776E-04 6094E-03 ------- *_ 8 0 . 2 .1 8 0 6 E * 0 2_ _ .7 2 0 2 E * 0 3 _ _ 0 . . 1 0 t* . 1 02 0 0 - 0 3 1 . 7 7 S 6 E 0 4 4 . 6 0 9 4 E 0 3_ _ _ _ -SOT -1.7324E*03 4.7157E*03 0. . .0 0 .6.3S27E-03 1,9849E-04 S.0a39bE03

C- - -T 1.A628 E-03 28 - *952E-03----.

,a 11T. 1.c-42JEvoZ - 26W0(03 -0.10. .4iOjiC.ia- 6.52-3 31 bOTI IoSI42E.03 5.36I1E-03 0. -O6~2~)iao .1521;E-03 31_ 801..-3. 19?.Eto3.... 2.4920.E.a33 ....... do I -.5jEG 2.6eE0 --1GE 33 EO.-.-.-0. BO. kS4.LE-03 1*515'JE-C4 9.606GE-o3

IFORCE AND NOTION OUTPUT IS IN GLOBAL DIRECiI AND, 2)

(Aj ~

- .. ' ~ t:L~ ~.~4 . -EL&E.

&.~~~~~ 11 AL f-,,. .raj - N-.a $aUALIT .693

J ..o.

SAll,', A.LI-nA. Am1L r..LCULAILL, IIH v'$WMAH4o

rn '.s * 1% * , iiI*... Ihs 1b Ct41C-u-LA i d IJHU(ss4Am

I------------------------------- CU~ai------------ ------------------------------ I

.- A :

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SECTION 4

Temperature Distribution of High Pressure Injection Nozzle *

The high pressure injection nozzle only has flow through it for two

conditions. One is a test condition when 60oF water is injected at 100

gall6ns per minute for 10 seconds. The second condition is during rapid

depressurization when the reactor pressure goes below 1500 psi. This

condition is defined as 60oF water injection for 45 sec. with a continuation

for 15 minutes at 400? water. The flow rate is 425 gpm. All other times the

nozzle essentially follows the cold leg fluid temperature.

The same thermal model and B&W Program 9116T were used in the analysis

of the RPI'(See Section 2). The figures showiig the transients run are on

i Pages fThese pages are followed by time-temperatures plots of selected

nodes and a discussion of selection of critical times. Finally the actual

temperature distribution is shown for the selected times for stress calculation.

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ITERATION TIME EXPLANATION

27967 4.95 Hrs. End of Heat-Up - No flow condition See Page 4-5

41491 7.5 Hrs. Steady State Temperature at 575 Hottest temperature in vicinity of Bi-metal weld.

42021- 7.6 r. Reversal in Axial gradient from 27967. See Page 4-5.

.39 6 8 0 - 10 Secs. Maximum radial gradient stress during test transient. See Page 8-6

15. 10.7 Sec. Maximum axial gradient in upper from start of part of nozzle Test

30 21.4 Sec. Reversal of radial gradient after test

12.1 140*8 min. Reversal of axial gradient in

after test upper part of nozzle

5060, 5063, 0-10 Sees. Maximum radial gradient stress in

5072 after start of radid depressurization. See rapid depress- Page 4-T urization

0 5124 1.015 a. One location of possible maximm

.9 min. after axial gradient stress. See Page start of rapid 4-T. depressurization

5237 1.0384 Era. Possible maxim= axial gradient stress

6059 1.2 hrs. Possible maximum axial gradient stress.

6307 1.248 hrs. End of 40OF water injection

6338. 1.254 hrs. Reversal of radial gradient and reversal of axial gradient. See

Page 4-8

6850 1.35 hrs. Reversal of axial gradient. .

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I -A 3 I s

* .

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o . I* s e s *. t* . I / , **.. . ID T

sq *

0006 9 4 1/ .

I II iA I ilt1 li ri0

.UTSIDE JNSI W I I SI SEG.FNT TI T? 3 T4 T'i SF1MENT TI T? T3 T 478 471 445 340 76 17 410 480 4P0 478 473 445 340 .76 1-- 40 4 3 480 47 r__ 3471 473 445 340 76 19 480 4.40 4r0. 4 47ft 47 445 340 7.1 P0 8 480o 4110 5 479 477 45 367. . 23 40 480 40

-479- 477 458 367 7%.47q 477 499~ 357 7 - 23 480 4 P.0 4.5ft i 8 479 477 4514 367 80 4110 48 9 479 47A . 46 408 480 4 80 0 479 479 450. 40 4 4 11 479 4.79 47A 450 9 7 480 *4 P.40 8. 480 480 48A 480 37' ?8 4 80 4RO 48 O

. 13 480 4An 48) 480 37;! 480 . 480 40. 14 80 . 44 g 40 7 2 .480 48an 4 S 14 480 40 480 480 371 30 480 4R0 48C Is4R0 4PA 48'4)

1 16 480 480 480 480 37n; 3 40 480 48 A.0 4

3 480 480 480 -.. .. . 34

-- - . . . . . . .

* ** . ."..~. .*

ITERATIor c0,3

TFMPFRATURFS PFP SFG14F.NT IJSFO) IN PFAK PRIrNCIP.F ANALYSIS

(IFUTSTDF INSIDF QUTSIE INSinSEflMFNT 3TI T2 * T3 4 15 SF1IMENT TI T2 T3 T4 T5

1 407 316 317 . 200 311 17 480 480 T510 3 407 . TR . 317 ?00 38 I8 480 480 inn 44r, 3 . 407 386 317 ?00 34 19 4A0 480 480 4;i .3 407 38A 317 ?00 34 10 4A0 480 4as , 439 - 419 352 225 3.. . *8 2) 480 4f0 480 .. 439 419 35? 225 38 ?2 480 480 480 4.

64-9 4.. 2 33 2? 40 4PAC 40 9 . 4511 4411 .407 2911*. 37 25 480 480 480 10 478 . 477 46? - 372 37 ?6 480 480 48(1 480 11 478 477 46? 372 37 ?7 480 . -480 440 48 *1?. 480 480 47A1 440 255 28 4110 480 480 4P .13 480 480 479 442 271 410 480 490 4

144 39 4 1 0 352 443. 334 3 480: 4 80 4 -,0 4 1.0

-458 4A0 ..40 .' 37 2 3) 4140 4 80 48 0 4. P

480 480 489 480 480 .2 480 480 480 4, p G . .. . . . . . 33 480 480 480 4i

*** ***.7 *.. -.. **.. . . .e..* . .

.- - - - - .

A . .

-e . *.es

-- - 4 N -- 480 4 48 4~4

- ..

. 0 006 I9 41 9

STRFSS ANA Y4I OF HIGH PP1r.fINl 1MIJFcrTION N07 11011K IlEHA1 IfN 5072

TFMPFRATIRES PFR SE6MENT USED Ii PFAK PRINCIPLF ANALY.IS

OUTSIDE INSIDF OUTSIDE INSinF SE.GMFNT Ti T? T1 T4 TS SF614ENT TI T2 T3 T4 Ti

1 245 230 1A.4 112 18 17 480 480 480 4A3 : ?45 230 184 112 Ift 16 480 480. 460 40 A

3 245 230 1P4 ?11 18 19 480 480 480 4PA.1. 4 ?45 230 1A4 112 18 0 480 480 4Jr0 A..,5 307 289 232 141 . 21 21 480 480 480 6 307 289 23? 141 21 22 4R0 -4A0 480 4P0 4 0 7 307- 289 ?3? 141 21 23 480 480 4:10 A 307 289 ?32 141 .?3 24 480 4 A0 480 4' 9 3A6 . 370 314 ?02 ?? 25 480 480 400 4r.,

10 465 45? 397 264 23 26 480 480 480 11 465 45? 397 264 23 27 480 480 -480 (o1 12 480 467 437 340 1 ) P11 480 4P.fl 480 0 4 13 480 46c) 441 346 194 29 480 460 480 4:'.. 14 '480 470 446 351 191 30 480 480 480 4,C 4r. iS 480 472 450 357 201 31 480 480 480 4G 4.00 16 480 480 4R0 480 480 32 480 480 480 4. 4^

.33 480 480 480 4F.0.

. . ..... . . *.. . .. ...... .. .. ..80 . .. 0*- .49

. ...... /

1E BABCOCK & WILCOX COMP/ Y

131. . 90r 0~ St OC 1522

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AE BABCOCK & WILCOX COMP/?

aS c * . 'I9. 9 o O C 1

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11~E BABCOCK & WILCOX COMPA

k17q 67

7t' ~ ~_ _ _ _ _ _ _ _

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' j 1.15 T *. ( e . . a Ia e .. . e 1 a , * . ':C& IY

* . .!. t 1* ATI 1

SECTION 5 ,osc 1522 SELECTION OF CRITICAL SEGMENTS

The following pages contain a sample temperature input and stress

output for iterations 27976, 6, 5060, 6307. The reader can discern from

this sample that the stainless segments 5 and 8 and carbon 'segment 23 (Bi

Metal Weld) are representative of the highest stress area Lthe nozzle.

Pages 5-16 to 5-20 contain a stress intensity summary of thermal stress

iterations runs. Iteration I on this sumary was run of pressure only on

the nozzle at a pressure of 1000 psi. This summary is for Segments 5, 8,

21, 23, 33. It can be seen that segment 33 has stresses less than or in the

vicinity of those shown for the make-up nozzle. Therefore, this point is

not re-analysed for the high pressure injection nozzle.

A complete analysis will be performed on Segmenta 5, 8, 23 therefore

justifying the acceptability of this nozzle under the design criteria. This

will be discussed further later.

C

C

CI)

8-7S -- ~,8 .7-

.* 00 IF U 04 2

STRFS9 ANA( YSTS OF HIGH PPFSSIRF TN4JFCTTON N01 "FfhN<F. ITF.1ATION Z7976

TFMPERATIRFS PFR SFG3MFNT IISFM IN PiTUtMARY + SFCONDARY ANALYSIS * *0* *** * * *** * ******************** ** * *** ** 0* 0* * * * ** * * * 0 *

AITSTnf TtNSTflF ilJTSinF TNSTOF SF(*4cNT Ti T T3 T4 T SFAMENT TI T2 T3 T4 T5

1 4cl? 4Q? 49? 49? 4i? 17 472 '472 41? 472 47? ? 49? 4Q? 44? 42? 49? 11 470 470 471 471 472 3 4Q? 4Q? 49? 492 4Q? 1 46A 469 469 470 470

t 40PJ 49P 49P 49? 4')? 9? 466 467 i167 46 ; 46F * 4'f0 490 490) - 491 491 - . A67 40.7 467 467 4-.7

. 6 4110 4A 404 4119 4'0 ?0 4(7 467 467 467 467 7 *419 410% 4R7 4AA .AA9 73 467 467 467 467 467

A 4$ir 411A 4147 4AR 409 P4 467 467 467 467 467 9 479 7480 4R) 40? 4A3 467 447 467 467 .4A7

in 410 .4Ai0 4810 4110 4A0 :)6 467, 467 467 467 4s7 11 4A0 490 4An 4R0 410 ?7 46 . 46A 468 4A . 46A

. 47c 476 477 478 479 A 469- 469 469 469 Als 1. 473 474 474 476 477 29 470 470 470 470 470 14 471 47? 471 474 479 30 471 471 411 471 471

1 477 47? 47? 47? 47? T1 476 476 415 475 475 16 47? 47? 47? 472 47? 1? 4P) 4 14An 4 a0 490 47q1

13405 5 4114 .484 483

*- * - . ... * ****** -. *** s..** * . .. . . A fS .4 44 . 4 1 4 4

.. ,*-.****.. . - *.. . . .- --.---

STPFSC% At-JAI YS1S nF HIG6H PIOFISI14F I NJFCT 101I NOV liFS*ip(F )TII.I1PM Z7976

* -PRTI4ARY *SFcomnAIwY srllFc~%FS

(HJTSlDE 11. 1JNI SI O)F

NO. LONG~ IMIP RAF). . LONG JIM >( RAn. LONG~ -HOOP RAI). * 3 . _9-0 -.0 .* -.0 -.0 -.1 -.1 -.0

3 -'.q 4.? .0 .5 ~ ?.3 10(. 1 )3.1 . .0 4- 11 8,.9 q _ PS 17 _0? -7.1 -7.4 -j3 -134.9 -5 L.3 -.2

9 4.8 112 .1-41.9 -)9K.,3 -;a -I8.13.4 -6S6.1 -41.1 -P.2 .365.? -. -08 .- 90.9, -1110,1 -74#.9 -711.0 -67S.1 - -10.6 614.Q. Q 540,.6 -14.4 9. -118.1 40 L; -7I)0'.0 -1213-4.

6:)41273. 15.6 -58. .1?. - 17.1- -043.7 -1135.6 . -16.C) 717 I9.9 -13 -?3.71 MI10 -4r-0. ~ -67-7.

1?A 1qn.... a; -1. A4. IQ. -11.0 -3 IS.o A -60R.9 -1?.?

I1C ' o7) ,?7 IPIH7 -16,.R .- 430.,R 49A4.? -13 -3MA4.? -4n3.7 3. 17. i 169.q Q IS 7. 1 -'. 3. 6-74P?* S 41A. I - -?0.0 -S900. 1.* -14?3.4 *..-41. 6

)A c;I7n."i 1977*1 -C;7. -q_571,6 1'N.? -170A. L- -62?62 -? -1963.Si -57.9 1Q7'41.9 * 5s6.9 -105.7 -39S.5 -?626.1 -76,1.5 -;339 7015.9 -0.

I__ P -91r,1.3 -2 47.4 -L367.W1 -13741&1 - 11 01 0 -?:336. 1 -2,01 16.0) -247.4 -. ?3 1866.6 11.1?6.9 1f0e6 .. 9.7 1671).l1 11.3 j 3'4?1 2027?.4 10P.6

PL -51397.9 U0PI.? 117.7 77910 7)??1je" AW4. 1 971 CI. R 121V06. 5 -. 117.7 -1117,A -Ifil.1A . A?.3 341.3 -'.7 43 .8 37*/As -2 h8. ,3 6.

26 -7&)l ci 4L4 9 _ n i, A 7S~li -8t993 1 91.5 . H941.2 -1)()H.7 - .8

P8 -1r.1.6 I S 2,9 1 .2 - .-9.7 -71.6 1.3 1631.1 106.4 1.2 71 ?C ; -no0. l).0 1H1.6 100I.f 60 30 0. 5 913.0 10.0

30* .15P.6 360, a 2?.3....47.6 31 C 46 *710 4) '1 It0. 3. ;I 2P.3 31 ?R.7 3495 . 13,,4 ?104 143..A Q7.7 -.9282.3 13.4 3? . 489.9 - -7.6 34.2 -63,9 -- 64.19 -. .3 -666,5 -259.8 3.2 iPi33 ?nP4 '-;04.5 1 -1 -13). -64S.6 -1?7.l -1150.0 -1436.3 -19.8

II~ITrilwI ordrt~, ve A, A I 'At ^. #-I., .. , * .,. . . . .

*ijj*

STRFSS ANALYSIS. OF 1IGH PPFSSIJPF 1I .FCTUIN WNi Iir.Fil 1IFRAITON Z'79c76

TFMPFI ATIlNFS PFP SFAMFNT I19Fil 114 PFAK PPUTTPL.F ANALYSTS ***********@*O******p1*********4on*a***o *n&o*n***on

(Y)

. OUTSTF' . INSIDE mnisAImiE TNSIlfF SF(MFNT Ti T? TI T4 T'S SF GMFNT II T? 1 3 T4 TS

1 4Q0? 49)? 40o 9? 4t) 17 7 472 41? 472 47? 2 49? 49? 44? 492 4i? If) 470 470 411 471 47? 1 4q? 49? 49?. 492 4()? 19 468. 4611 469 469 470

4 40? 4'op 4 4 44? 4c)? ?n 467. 67 4!7 4AB 469 ; 490 49? 491' 4wl 1f 46. 467 4f7 467

6 AA 418 489 489 400 ?? 4t.7 467 467 467 A-7 7 486 44A 4A7 498 419 71 467 467 467 4A7 467

8 486 48A 4h7 4145.. 419 P4 467 467 467 467 4- 7 0 4nO 14A n 441 411?, 4A.1 S 467 4 67 467 4f.7 467

10 4140 . 4t0 484- 480 45) ?A 467 467 467 467 4h7 11 4A0 48R 480 4110 481 77 46A 469 46A 41 A.A

1 479 476 477 4 479 PA 46 C 469 46 464 4A9 9T 473. '474 479 47f 471 ?9 470 470 470 470 470

14 472 47? 473 474 479 -i 471 471 471 47) 4/1 1 472 47? 47? 472 472 TI 476 476 475 475 479

16 47? 47? 47? 472 47? 1P 4 811 41R0 480 4A0 47P 3 4f.5 4R5 484 4 64 4A3

.... . .. *

00061I9942)

STPFSS ANAtYSTS OF HIGH PPFSS1iRF IN.JFCTION N07 AFM11tiI ETTIATJON Z71)76

PF AK PP (NCII*AI. $Ikf f,WS

: FC1 OT.S16F M r IWL ANF* INS IfE

NO. LONG MOPi An. Lnb H0,P RAn. LONG 9101W RAP.

3 . . -0 .0 ._-.,. -.1-.

? -. 4. .3 13.1 0 4 4.0 7, -7? -7.3 --1.3 -1149 -1.3

* A non. 61.2 - -3*73. 0 -1 19%.,4 1 -?'.6 -1tli6 i-724.7 ___. 46 6o 1 ?fll7 -~5 -33.R -n . ) - 7 C) J -7S?.1 -7 16M. -9.5

Is 67 .? - ?0l's -14.3 -:3,. 4 -3'P. e* -H6. 4 -1?33.1 -14. 9 -?4)fl.4 3q6o3 .- 3 -20 1346.1 11-I I. 7 -3 .4 -61.0 13

~ 100,0

9 -7 ?). 9 . , .- . , K . 4 . 3 9 4. P 6 3- . )7,? -49.1 -4,.4 1'J*4 17. -A.1 -411.9 -'i4c, c? 1? P ?A) S f., n6. W -14..5.....-17.1.....7? .3 -q,. 0 -V.6. 3 -610.3 - 19.5i 13 !;fl1 66n .5S -?4.5 -10 In6.5C ?sc9.19 -16r, o4 -9?9.0 -4 h4. 6 -2 4 9" SI.__..P14.4 976.,0 -PA4.4 -P70.4 101103 -70A.1 -?916.9 -IO8H.2 -?A/

I1C i~I I pIP 0 1 -'160? -43. .'. -?e3 -511.2 -14?.0-3? 1fl7 P.p 115. . -5.7~. - 441;.? P 3 -L)r 11 .4 -i;r .(1 -3 JAC 7o7 17,. 57 -69A.7 A(-. *' -377.h -6.181.3 -?079.2 -57 .7" 19 - 74 1 c.? 4n06.3 -1r1fi.4 -ROR.3 -2997? -7 0'.. -9 3fil.6 -7164.0 -10.4

21 ___ 4- C5'3 -9 1 CI. 1 -247.6 -545;.5 .171 V* -I 7QL). 4 -23?"1.f -20114.'; -4. 23 aSil.9 )41'4.0 100.7 n~s. 1671;1-..h "I.A -3 H.S? . ; 202?74.7 100.7 -"1. 30n0.5 117.8 779.31 72 19.l h Slit..3 97?3.9 1;'1 4. i 117.8 -3s.6 -13. ?*3 3610? -9hP(- 4 43V,. H 3771i. 5 -a 5. 62.1 76 -- -~~ 4 -113.4 H.6 7%.14 -AqL;,4 5i~~ 8'47.7 -q98.9 .14.

? SIP 1rP71v2-9.7 -731"3 3A.3 16P.7 106.1 1.2 79 ?.6. -0. 100 6. 1. An. 1 299.9) i)3.? 10.0 10 7)d.9 36.3 . S'.3 ....60.7 65.7 13*2. 54 1 4. 137. - 39.3 13..2

"l? 5RI.? 5.

1148.0 543192.. 1.5 -7.1 ?6.6 -604.7 -206.1 2.7

319o 97r15.02 210 .1395 . ,1- 0 .

TV**t1F ill: 5 P I' i r(?4,; I I1I l 1 tPIA'Y * '. II-miIAI(Y ArALAYSIS

flJTSTPF INSTD)F AUTSIDE INSTIF SFrifrtIT Ti TT T' Ti VFA4FNT It 1 T 3 T/ 1 1 it 1? TA4 VA PI3 1.An 17 -t80 480 A 80 480 4q0

47? 199 3?6 ?53 180 1' 4110 480 410 4180 401 3 47? 3g0 .?4 ?51 1w) 1 480 4 A0 '01 480 4A 0 4 4 7;? 39) 176 .?53 190 ?0 480 480 4AO 480 40 Si S04 42A 348 ?70 19? ?l 480 480 480 480 48A A 504 426 319 27f 1) £480 480 480 4 P0 4 Fln 7 504 4?A 3 A 27tt Ice? 14 R 480 48 0 480 . 504 4? A . 31 .?70... 10? ?o 411 480 480 010 480

c2?7 454 38? 3og 7 PC; 480 480 480 480 48.0 l 49 4A? - 4)% 341 PR) 480 480 480 4R0 480 11 94) 48? .41S 14A6 a' 7 480 480 4!50 480 480G . 1 27 _487 -. 446 *. 40~ .. ).. 48.0 480 4FG 480 41A 11 5?7 487 447 407 167 480 480 480 480 .480 *14* 5?6 4R7. ..44A 408. . 3 .0 480 40 ... 490 480. 480 15 926 487 448 410 371 1I 480 480 480 4P.0 480 16 . . .... 4i0 ..480 4h0.. . 40. T.. 480 480 . 480 480 4A0

33 480 480 480 480 480

.* . .

*. .--...-.. .. ..... .. ... ..-. *... .*... . .... . . .

(I.'

R4 A 14Y + SFcomnfA,,Y SIf -G rF

flI'rS111 M4 I OVI. A VJ TNSIDF

!n,. I of"A ~Iflfln PAD, [LONG l110OP p4m. LONG H-oop PAI).

. -4 n1'i6o ) -0)7470 1104~1 4cc,4 3I~.) fl-cJ CSIf,3MR4 10.

7c? 4 ,9' 40 7C1. coOb 0 4AIs)97,5 k l?6.4 760nl.3 551~~)*q .6 5,147,6 1109. 0 4 1 /'.9.? -/o4-ji9?. 11 (6.9 .4?17.9 162?.0 S6307 .7 56413.1 110IS.9

-C~)AIc I. -SfI1." 114:1.7 47166.9) -P ,?. 6 7 i3. 2 h70(,P,9 511116.0 1143.7

Ai -q7>940.4 -'l'97(.f0 I 12p, I C.) 3(t4 1W??4.90 114 36 7. 54178 . 9 122.8

7' -61 7Mn.4 -569n e c 1'"-4.e 314. 71;47.6 9 dM.!c, w74i 718?7.5 6330 1394.7 A 7Cnfir( ;.* -I7A.? *141%6.6 6?0'9.7) 41af V7. n1-3.' 4. .506. 7 -1466.h.

-1'04. -6?9 7.1 Q A .0. 1 ;1% 74. .4 8477,h 5().' 11O4?.? 16P7. 5.0 -_ -1 -4c. -5A647.40 P1 14......4A9,7 W.491. r V -5. 0 f474750, 5-73.? ?1.4

1? - 641 -96047.1 1807.0 -7?i1 .6 -1?)!0.3S 11664 .3 8 3r6J7.2 3?097, -281.0 1__ 71 1?7.40 -P l417I 161 413 41A6'0 .3 706.6 h5l?. 304 . 3049.0 13R6.1 Is - I7311. 4 3IQ?' A. A 13r;,837 7.67 3 7(.? 4 *1 (3 185496.5 11946.1 13.7%

i r _ -700-1.9 -)A~46.?A I?;Y 59.9.* 449, -Va. 420ni.4 310.3o 40.9* 1229.9 17 -InO9*4 -81. ;.1 0 174,4 -Yi14 .4 A6.9 77s.2 -26.6 9.0

.70q~ -3.5 74 1..17- 4 54. 21 -6%.R 4747,5 .-633.2 -3.5

IQ.? 13. -1.6.....j-14.3....,) -1 t. 1 ;.-t 1 1.. -74.7-. . -.6 I3A, ?n73 0 ,1 1v3.6g, -*AP.R -62, 7116.1 -31.2 -/64.83 112.1 -r,.68

? c?.7n 11.9 A0 ,1 -0.4 16.7 66.6 -.7 10A4.3 -.1

?LONS 7331TqA1 .DRC?1N IS )03~f.7S~L 676SIQF.6 71 (1.)A 78RCIO IS 0O'A TO SHEL MIDSUq~iFC103.

TF:MPF AII FS PIigO ',h i+i ill ' I ill, I It CI ).F ALIAt.YSI I

11JT' II N'11F 01i Sil I NSIOF.

SFqrt rrtT [ ? T3 I' 1i AiGIiFNT TI TP T3 T 4

1 4PP 40n 3S 17 1i 17 4410 480 480 480 480

4 40c; V9i ?60 1?I. 18 480 4R0 480 480 480

3 4?' 40' 353 Mir1 1') 4110 480 480 480 4ft0

4 4PP 405 353 ;I60 1?7 0 F lO 480 480 480 480

5 447 43P 380 ?"0 1?I ?1 480 480 480 480 480

6 47 41? 300 PAQ 1Pon 480 480 480 480 480

7 447 417 381 P 1# 4ki0 480 4180 480 4'F

* Mt? 43? 380 ?2it .1? ? . 4 480 480 480 480

..... q . - 454 4PI 331 480 480 480

104 477 46 ? 1 7 t . 0 480 480 480 480

441 Itll4 A 382 12 S7 21104n 80 Al80 460 4 A0n V 7r. 48074.40 2.. .6. 43. 24 .... 0 460 j .480 4A0 48 44? P-31 480 4840 40 40

... ..-* *. -.

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t .- - . . .. -..--- - . - *- - *.-- . . . . . -. . . . ..-. . . .

. . .. . .. :. ..- -..------- --- - -- -. *-. - -. . . . . .

1. ..... . .OM ...... .. * *** 48, * *

** .

I~I

III) 0 ~0 0 sggoa 11)

nur9nF M IDi.. NF INSIDE SFr,. 11o. I OHij HOp RAF). LOW HO4)1 Il A. LONG IIOOP RAI.

1 1 .1-0I0. 111 1.3 -549.7 -. 371. 5 1iii.8 74996.8 790?0.1 1115.3 P -31917.A -311.7 1115.3 -)60,. - ..1 71381.6 7498151.6 75014.1 111 i.3 3 -11q63.Q -TINA1.6 I Ill.2 -5547.5 -'A..i 73i7, 8 75034.5 749A0.5 1115.2

4 -3178.7 -3).17fA 1117.2 -s23i.A -64.09.6 7402.2 759i0?.3 75573.1 1117.2 c; -___ 6fl.f 1 3 -32?9q6.? 1167.5 -4700.2 -13'4410..1 ItiHA.? 10419?.5 85987.6 1167.5

6 -37?04.5 -33793.1 1368.1 -j4??.1 -13476.- .6?0.h 841c8.5 80912.9 1368.1 7 & S41Af.7 -352;4. . 1416.8 -5797.5 -Ilr'9. I 9lv9t.l 941 L2.5 85767.7 1436.8

6c 96?g ,.7 1-70Q7f'A.9- 1403.S -L;374.4 -1 18611?.6 9)r 6l.4 116')17. o6 93994. 1 1903.5 -1460.7 -19767.5 1871.9 813I.A -17;1.4 ))0 a*/A1i.7 9')071.c 1871.9

1.. -l41.A -IsAI. A ?S)1.A -I I )I1.S V) 4 941$6.3 109508.6 211 - ro')9. f -014 0. ~* ?7-11716. .-1 ;471. 4 $'~1 61c;1 464 43 ft 1 ?(1 19 ?911? .7

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14 _ 16911.6 .- 10?2o.~ 11'. o -905A7,7 -A Fs W/ h 419 0o 676'4.5 794W1 .9 215,;.? gE~~~~7*7~~~ .. c4 _ Oi. Q~. ~hti7 mob-614 4.2 747 7. (1 2 0 A. 5_

17 --7596.o -%s-sf n.RA 19 74A.4 -4672~.0 146.0 9087.2 -3916.7 31.9 18 AV. -4467.9 __-11.5 P66,7 -;Fn.~-142.6 273?*9 -61996.8 1.

P 1>4141 c -q710(... -?71,.1 -7n?.n -1 4tj141, f -?nll.6' -3436.4 -22105.8A -27A.1I R'__ ?3 C;. 14201. A 3. 1 -1I6 *0 _163,17.1. 61n . -56 10 6 - 19123.0 .. R 3.1

-750~j1,0 48. fb0 6?.) *3.50.2 8696.3 12030.110. -1~ 36c;. -167?*4 110. 3*7-50. 4 4?.5. 31q1.2 4.9.....60u5 ?-7n4 -A?]. 19.0 f69.5 -141:,1 56.0 767.8 -8345.8. 9.0

P" 44q*6 .1?.8. 4_ **~. .1?I0 *?4..-27.8 . -4Si7,6 -489.6 -31.6 _

11i. .7 7 36 -4i0 -~3 _pc.2 -169.0 -101.7 -. a ?O ci4*....:R----17 e..-1. .....-'4 -10.-9 .~.-75.5 -9.6. -.1 .7

3n P-4:5 1367 -6 -6.8A 715 -3.2 -3?.6 11.3 -w6 ~ 1-~-10.9 *..1. __ -. 3 .a R0I....-6 ... 1..- 15.0 .-. 3

P? .6 9.0 9 . 4 6.1 7 8 -. 7 10.4 -. 1

IT

j (LONI1iflNAL. rOJRFCT1.0NA.S .ALONG. .SHELL- MflI siRF ACE. .r0)L IECJIO0N..IS NORMAL TO SH-ELL t4JDSURFACE*V

14

17 19

o 0 SI 1)/3 Ji I Ut

TFi MPFRATIRES PI.9 SF6MFNT USFD IN.PHIMARY * SFCANIDARY ANALYSIS

nUTSInF INSTOF OuTSIDE INSIF SFAMFNr TI T? TI T4 IS SFGMENT TI T2 T3 f4 TS

I 5sA 475 391 30R 2?4 17 480 480 4A0 4110 480 55R 479 391 308 ?4 18 480 4P0 480 4io 480

3 -59A 475 391 308 ??4 19 480 480 489 4A0 480 -4 5c;15 475 39 308 ??4 20 480 480 4H . 48) 480

5 560 48? 404 326 241 21 480 480 4aq 4A0 480 6 560 48? 404 326 247 22 480 480 480 4A0 480 7 560 48? 404 326 247 24 480 480 410 4A0 480 7 560 48? 404 326 247 24 480 480 4FA 4 *0 480 9 554 487 421 354 ?A 25 480 480 480 48 4 A6

10 547 492 437 3R3 311 6480 480 480 480 4041) 11 547 49? 437 383 Phi 27 480 . 480 480 480 4F.0 1? 498 485 471. 457 441 - 480 480 480 4140 480 13 498 485 471 457 444 2 480 480 480 410 460 14 49R 4A4 471 458 444 30 480 480 480 4 A0 480 15 497 484 471 458 445 31 480 480 480 480 480 16 480 480 480 480 4832 480 480 480 4P. 480

33 480 480 480 480 480

*..

0 0 0 19 0 4 . A s 'JN 0 000

PRIMARY * SFCONnARY SrHkSSES **************4**** ***** C

OUTSIDF MIDPLANE INSIDF ISEct. NO. LONG HOOP RAD. . LONG HOOP RAn. LONG HOOP PAD.

1 -56571.9 -56963.4 1296.5 4770.1 4AL.0 8651.7 63518.0 63536.9 1256.5 2 -5657?.3 -56572,2 1296.5 4770.2 404,6 8651.4 63510.6 63524.5 1256.5

- *56700.0 -56566.2 1256.9 4717.7 456 ,8 8654.1 63661.0 63633.3 4 -9q798.1 -561?9*0 1256.3 47??.A 66511) h651.6 62638.3 63964.6 1256.3 5 -61. S -60614 .9, 1-57521.0 12)9.8* 5058.8' -?.354 0~ 83518.6 68 193. 11 58692.1 11.

51951.5 -54?44.5 1323.0 5043A 2163(s 9034.2 59439,5 .56677.2 1323.0 -59818.5 -55970*2 13AIe01 943S.6 68316,7 60481.5 1381.0

8 -69323*1 -56.10,6 143A.R 60?3.6 -444A 95A3 6.2 74534.6 633?7.5 143fl.B 9. -3c;717 .6 '-3RS 14 *3 159501 *93R4.l 1 74iO 10777.3 43760,2 59049.4 1595.1

10 - -21077.5 -77990,0 1773.0 S343.4 5172,4 11667.2 30613.2 4780q.5 1773.0 11 -2?R30.3 -26Q71.6 1018.7 5359.4 6414.9 11805.4 30431.8 49393.6 - Il.7 12 -1186S.9 -2 6 . .D -- .- 4- 46O.0 1? -1515.9 1?~6.~ 1160.0' 4S22.3 -2681 -@I 49?. -8381. 1.8 100 13 -7378.9 -A10,3 449.0 155094 -1074.5 2510 9595's 8639,1 449.0 14 -P749.4 -6064. 434.6 1007,4 11?3.7 2818.1 3843.1 10008.7 434.6

15 -4-10.2 -99q994 ()'3. 8 15-40. -94.9 3947.8 6;3.9 I1-. 1 2534.1 - 4. 905. 3*. 17 -3hq.1 -989.8 "10.6 24.3 -1?4So3 -86.3 416.5. -1658.1 -10.6

-- 2236.0 -677.4 -33.7.-238,2 -1791.4 -?41.2 -2744.8 -3478.5 -33.7 19 71A6.0 -111RIA -100 -777,1 -4107.2 -693.9 -8801.8 -8768.6 -100 20 7013.9 -4723.0 -19R.6 9265S.-Q 0. -1404:2 -8750.3 -16464.8 -198.6 21 19A9.5 -9513.P -29.7 -621,6 -1444'.4 -15195.9 -2624.1 -21273.6

~ 3 -4?50A.4 142(69.0 9.R -11 .64 167114. 764.4 -445') 1935.0 9)3.8 2 - -8084.? 32A4.5 113.6 74.4 7393,6 856.5 93h?,0 12178.4 113.6

-'-'-34 Q.0 -15106?.1 362.2 -A13.2 -414.5 37'3.5" -143.95. 6?.1 76 -639.0 -866.9 8.6 66.2 -847,2 52.6 72?.3 -903,4 8.6

27" 411. . -26S.5 -30.1 4-499o6 .9 2A 136.0 -4 -3.7 -26.1 -51.0 -26.1 -174,9 -101.8 -3.7 29 56.2 9 -1.7 -11.1 -77.6 -a.6 -1.7 30 23.9 14.1 -.6 -7. 8.0 -3.2 -33.3 12.2 -.6 3S 1 . 0 1 2 9. . 4 7.2 .. ,061 5

3 3.5 9.0 *1 44 61 3.3.9 -56 10.623. 3123 6.9 11 0 40.5 220 -223A 6,7 -T0

-8V.. 44. 90. 17.

C66. 346 10.4 12.

0006 9 4.;3

TEMPERATURES PER SFG14ENT UISF) IN PFAK PPINCIPLE ANALYSIS

OUTSTDE INSIOF OUTSIDE - INSIDF StGMFNT TI T2 T3 T4 TS SEMEFNT TI T? T3 T4 TS

1 478 473 445 340 76 17 480 400 480 4R0 41A0

2 478 473 445 340 76 1s 480 480 480 410 480 3. 47A 473 445 340 76 19 4.90 480 480 480 480

.... 4 478 473 445 340 76 20 480 480 480 480 48R0

5 479 477 459 367 74 21 480 480 480 480 4F0

6 ;479 477 45A .367 74 22 480 480 480 480 4P0

7 474 477 45A 367 74 23 480 480 480 480 480 a 479 477 4s 367 74 24 480 480 480 480 480 9 479 470 46 403 86 25 480 4q0 480 480 480

In 479 479 478 450 9 . 26 480 480 480 480 480 11 .479 479 47P 450 9R 27 480 480 480 40. 480

127 40 .40 480 480 370 28 480 4e10 480 4P 6 480

13 4R0 4130 480 480 372 29 -8 - 480 480 480 480 .480

14.480 480 480 480. 373 30 480 480 480 4P.0 41R0 5 480. 400 480 480 .375 31 480 4A0 480 410 4r-0

.480 480 48 32 4480 80 480 480 33 -.. 480 480 480 4P.0 480

.7. ...-- . .----- -. *. .

.. ... . ..... . - . . . .- *- - - - -

,-O~-- - ... . . .

PEAK PRINCIPAL STRFSSFS

OUTSIDE MIOPLANE INSInE

NO* .ONG HOOP RAD. LONG- HOO-7 RAn. LONG HOOP RAf*

1 -?7541.0 -27511.5 1554.3 -15022.3 -18992-1 7 070.8 116998o3 117022.5 1554.3

2 -77540.7 -?7539.? 159.3 -IS0??.4 -l0?.2 770.5 116995.R 117009.4 1554.3 :1 -7610.4 -27S43.5 154.6 -15014.7 -1P61.6 707?.8 111.7 117104.9

4. - .9 -27003., 1554.5 -1061.5 -I 7073.5 116274.4 11712.6 S -41079.7 -21849.0 157?.6 -14925.9 -213F6.5 6S91.0 1440

-??647,9 -?4317,.9 11101.7 -15 130.o5 -?1 049.4 h654.2 '1 ?21 S7 .7 12.0l99.8 1s()1.7f

2q Vio?1o;0 -29329.8 114S3.6 ;-14664.7 -14861).6 701c-;.7 12c'573.0 123913.3 1853, 6 A -S1361.5 -20006.5 19n3.2 -14314.2 -18400.2 71361.7 14o26q.6 130,i43. 4 1 c)03.2

9 - -6711 .6 -11596.1 2300.6 -12467.8 -13271.0 7n77.4 I l68b1?*6 127442. 8 230 0. 6 9n -39.3 -4678.0 3021.6 -10500.4 -10790.6 524.1 117164.4 12R921.4 3021.6 I33365.0 -11173.5 -1063.2 353..7 116620. 13096.9

12 -529A.3 -51?7.R - ?lR5.7 -R19.6- -6634.8 2194,1,- 433?0l9 32G04.4

*14 4105.1 ?86.6 94R.9 -2169.0 -2264.2 32S.6 30707.9 35818.6 94A.9 19 4977.5 1120.8 901.2 -3007.5 18?4 9 I 122.11 281 63A 35265.3 901.Z

17759.3 -3096? -11.8 -97.4 -754.8 -121.5 -933.8 -1361.6 -17.

I8 A 796? a0 -47.5 -37.8 -319. 1 -127901 -261,5. -3613.0' -3000.6 -31.8

19 7301.3. -940.S -98.8 -7A9.5 -3736.0 -690.5 -8932.7 -8269.7 20' 6Q47.1 -4611.7 195.5 -914.3.-94?7 -1380.4 -9664.9 -16214.6 21 1919.7 -9500.6 -257.3 -610.0 -14364:3 -187A.2 -273R.5 -21142.0 257.3 23 4131.0 1285.7 95.4 -11.2 16784.9 775.7 -4510,6 20n60.6 95.4

?4 -R171.0 3257.1 756,7 7343.1 864.5 -3348.2 162.3 362.5 -06H.3 436,2 3791.7 -164.8 62*3 -e -718.6 -840. 5 1 .65.8 -8$i?.S 52.1 716.1 -91?.1

27 467.9 -113,8 -30.6 -266.4 -3A.5 -501.3 -3.9 2A 136.7 -3.7 1 .3-51.0 -26.2 -109.9 -3.7 29 56.4 14.8 -1 -1').0 -1.6 11.2 -77.3 -R.4 3A -24.0 14.2 __ -6-7.n 1.1 -32-3412.3 -,6 _

30O* -2.3

-2_9. _ . -92.4 -100. -37.2 1199.4 1109._55.

11.0 13.5R 1 .6 -1.7 -10. 7 -.6 -1179 15. 1 .3

3? P. 2 9.0 5 7.6 .4 69 .09 -. 1.5.7.10.6 -57

333 .97.0 -.0 -1. 4.6 1.0 124 6.7 5.0

(LONGITUDINAL D1~T0 SAOGSHELL'*14IDSURFACEv R..QIAL'DIRFCTION IS NORMAL'TO SHELL MTDSURFACE.I.

-20065 90.2-14142 18002 7617 49656 1053, .193.

S-11506.1* 230.6-126.8-3210 07. 18. 17428 2.-.

-47. 02.j190, 1706 2011714418214 32.

TF?4PERATIIRES PER SEGMFNT USFO) IN PRIMARY + SFCONflARY ANALYSIS

OUTS~nFl INSIDE 011TSIDE INSIDE

SEG"FNT TI T 'Tl T4.- T5 SFEGNT 11 T 2 T 13 T4 T 5

1 0000 0 17 69 68 66 65 64

2 n 0 0n is 69 68 66 6

3 0 0 - 0 __ 0 _ 0 19 99 97 96. 94 9?

4. 0 o n 0 -0 ?0l 129 .1?7 325 1?3 1?0

.- .0 n 0 0. 21 119 139 138 131 136

*6 0 0 )0 0 2? 139 139 13A 137 136

70 (1 0 .0 0 231 139 139 )3A 137 136 000000 24 159 18157 1561 s

9. 1 1 1 0 20 ?00 197 - 19L 12 11910

t10 3 2 1 0 -) 6 ?30 2271.? 2?1 218

I11 3 ? 1 0 -1 V7 ?60 257. 254 25n0 247

S... ~ 12 16 13 1n 7' 28 ?90 2AS 281 277 ?72

__13 29 24 19 **~*13 3 31 314- 30R 303 2cj3

114 ~ 4? 3 r 27 2012 .30 348l 34? 336 330) 323 15C 69 6A 66 65 .64 31 377 .370 363 356 349

16 69 . 6A .66- '-'65 64 32 407 399 391 383 374 I.- ~- .33 436 427 -418 409 400

PRTMARY + SECONDARY SINFSSES .

uMIIPLANE. INSIDE

NO. LONG HOO AD. LONG HOOP RAD. LONG HOOP RAD.

.0o.0 -00 .0 .0 1 *0 .0 ._ 2 -0 0 -.2 0 -. 2

3 33-.7 .0 .4 .0 3.8 1.6 .0 .30 -0.3

4 11.4 .0 -7 -1n -145.9 5 10?.4 -4.0 -.5 -3.

-6.4 -135.3 -R.1 5.4 -205.9

.9, -181.9 -24.9 -.7 Q.0 -?43*6 -5.8 P04.5 -239.0 -,7

8 -374.1 -341.4 .4. .1.6. -8$flo4 1.0 419.2 -?30.? .4

9 -44'. n -669.1 6.5 67.2 -301A 40.4 99494 155.9 6.5

10 -1272.? -775.4 ?4,9 153o1 -31.Z 157.6 1599,4 1049,4 24.9

11 -AP9 -73?.? 44.0 '25119 ?1'.:3 ?A718 2134.1 1506.3 44.0

1? -315 20. 1.6 .455.? .1517 ~2o.5 423'e.4 290.3 St.6

13 -8.0 -3371.7 7?.Q 8436 9355 7481,4 70270 172.9 14 74391638 7*.32.

14 *- -6'',3 -1000.4 _312.3 1016,1 462'.1 .2061.4 7431 107.323*.

15 -4848*0 -31tR.q 200.0 1079,6 -?766.H 130A.0 4 1.r -'3292.4 200.0

17 -4453.4 -IS9?*R 14060 41712 -244915 211.6 53S6*4 -1223.1 11 -?531.0 -11iQ512-- 4A,.2 395. -.Is 301.4 *304003 1321.3 .48.2

19 1279.0 -IP1643 ?3.8 -36.1 -196?.0 147,3 -1559.6 2535*6

20 79$6.1 -3546.1 -3Ae8 -311IR -476R.S -299.0 -3699.4 -6811.5 -38.8

21 148.? -4h5g.9 -93,7 -275.3 -6747*3 -703.7 -1961.9 -9009.9 -93.7

23 ?P70.7 193to4 15.0 -165.4 4287.1 131.8 -32?3.0 4;40712 15.0

24 -1979.1 qnlR.9 3?.? 174.4 2397.7 24?.3 2306.2 4244.4 3?,2

2. ' -1?1 7 -13R3.8 47.6 290.9 51.0 0 3120.9 3766.7 2905.8 47.6

26 -1019.4 -P9 4H.5 ?79.4 -1?77.4 09

27 -?AQ.7 -2773.0 92.2 184.? -154.9 603.7 2695.4 1613 2 9?.2

129 -?14S.0 -?6132 163.6 338,0 .68~4,S 1040.5 2081.4 5L973.4 163.6

2c) -1902.4 -279 234.3 1487.7 2439.1 6867.2 239.1

30 -912.? -3?4?.6 2A3.6 5?P.6 . 1693.1 1838.4 6063.I 283.6

3) -467.7 -1067.4 205.7 2q4.') 0., 1?37o4 909.2 5205.6 205.7

32 1123.3 -213.0 ?19.0 144.3 259.? 1333.0 -1313.0 3204.4 219.8

33 .604.2 -4118.0 10.7 -lqs.8 -3345.3 841 -3643.2 -4040.5 105.7

(LONGITUDINAL DIRE.CTION IS-ALONG SHELL MIDSURFACE. RA)IAL DIRFCTION IS NORMAL TO SHELL MIOSLJRFACE.)

.~. .-. 7

0 . 9 0)~l 1,

TFMPFRATIJRFS PFP SFGP4F.NT IiSM-f INI PrA K PRINCIPLF ANALYSIS.

0 SC 1522 N

(MJTSIOF T...T NSTrE MUTSIDE I INS I U

SSFT Ti 1 T2 T: 11T l ~rET *lT T3 T4 7 CS

1 0 0 0 0 0 17 .68 6SB 66~ 6c; 6

p 0) 0 '0 JR 68 68 66 69 65.

3 -0 0 0 0 0 - C 99 9R q5 )4 920

4 0' 0 a 0 0 20 130 127 13925132

5 a 0 0 0 0 ?1 145 137 136 13R 137

6 0 0 0 0 0 '22 145" 137 136 313

7' 0 0 0 0 0 234 145 137 .136 138 137.

9. 8* -0..( 0 0 0 0 24 160 158 157. 1 t;6 155

q 0 02P.5 ?0q;1 .IC

3 0 ?6 230 227. 22

31- 0 0 27 ?60 2937 255 250 247

15 131 ~3 PR 2 89 28~5 27 -~ 272

13 2A~~~ 24 20 13 7 2c) 319 ~34 309 .303 -298

14. '40 3; 30 20- 10 30 348 342 336 329 323

15'~ 68 68 66 '65 - 65 311 377. 370 -3 . 3S6 349

16 6R 68 66 65 *65 32 - 407 399 391. 382 374

-........ *436....427....418~ 409 400

PEAK PRINCIP4L STRESSES

OUTSInF MtDPL4NE INSIDE

NO. HOOP RLNG HOO' RAN. LONG HOOP RAD.

1.0 .0 .0 -.0 .0 .0 -.0 .0 .0 .2 -. 1 -.0 -.0 -02-.0 -.2 -.4 -.0

3 -1.4 -.7 .0 .2 .4 .0 1.7 .0 4- 11.6 11.9 .0 -. 7 10.3 .2 -13.2 8.3 .0

-.5 -5.9 -91.4 -3.6 *139.1 -194.0 -.5 -7.6 -137.2 -1.1 -1.4 -168.8 -1.8.2 6.7 -207.9 -1.1

-187.6 -251.9 -.7 9.2 -?4 6. -5.8 208.7 -241.5 -. 7 A -481.5 -311.9 .4 22.0 -290.8 1.1 508.6 -208.6 .4 9 -879.4 -697.3 9.7 82.3 -29e.1 44.7 813.0 40.5 5.7

10 -131A.8 -8)5.6 21.6 1R4.2 6.6 171.7 1336.? 817.1 21.6 11 -17ocl.6 -7A1.7 .TQ.2 285.9 253,1 Tas.,0 18164.6 127..S 31. 2

1? -1070.A -?1r4.7 77.8 173.0 -431.6 52P..1 4366.2 310.9 77.h 13 -q?7A.4 -?8?1.5 370.9 23R.? 31$.1 1087.5 8016.0 7524.3 170.9 14 -4842.5 -1027.0 312.7 C) 2.8 .3700.3 2000.2 8439.9 14803.6 312.7

15 -19.9.? -3489.5 193.2 1220.9 -2613.2 130'1.8 6149.8 -3155.8 193.2 17 -4195.9 -3287.6 26.4 6g6.5 -2?7/8.'4 ?75.8 4988.6 -1531.0 26.4

18 -24 7.1 -1117.9 35.2 476.5 -14.9 35.0 2739.0 1031.1 3.2 19 1311.3 -1703.6 16.4- 54.9 -1R7.2 181 -1 94.8 -2574.8 16.4 20 ?790.7 -37?2.4 -35.5 -312.1 -4751.1 -307.6 -3500.3 -6608.7 71 -48.9 -669?.4 -69.4 358.9 -6097.9 -785.1 -2277.2 -10102.0 -69.4 23 1393.2 ?4)5.9 .36.1 297.1 4750.0 51.5 -3417.2 4604.3 36.1 74 -7151.2 7?R.3 43.9 177.7 7406.5 201.2 2262.7 4208.2 43.9

-1160.4 -1475.6 48.7 184.0 4A7.5 3?4.4 3672.8 2R16.4 4PR.7 ?A -140 .1 -27A4.6 48.1 56.7 -1491.5 324.1 3410.5 518.4 4[.

27 -?46c..7 -?c44.1 90.4 -164.1 -500.3 607.3 2690.3 3611.6 90.4 28 -046.A -2530.9 161.1 45.7 392.6 1043.1 2879.? 5972.6 161.1 ?9 -1424.7 -?67?.6 236.8 240.6 598.7 147n.8 *2440.2 6870.1 ?36.8 30 -854.6 -3182.2 281.8 342.4 13.9 1683.4 1841.4 6069.9 281.8 31 -42A.A -12?5.6 204.4 174.4 766.2 1?27.7 908.0 5212.2 2C4.4 32 1145.9 -2111.3 219.0 83.1 201.4 1327.3 -1316.6 3290.2 219.0 33 . 143A.5 -4462.2 105.4 -1!7.6 -3344.1. 582.2 -3651.4 -4039.7 105.4

(LONGITUDINAL DIRECTION IS ALONG SHFLL MIDSURFACE. RADIAL DIRFCTION IS NORMAL TO SHELL MIDSURFACE.)

a .* *

0 0 6

TTFR PaTmaHy sFCONInAPY Syr*FSS INTF1TrrIrT I-.A Surss IN[ENSITTS

L L- P P,-0 11L R. 4

IN;1nF1 0117TR1 nF INSIOF OUTSItsE INSTfF OUT!inF I.Slol UTiS10F INSI1OF QUISIOF IN;IDE 0lT'S!r

3 94.1 -51.6 -S0.2 50.9 -7*Q 27 1041 -42.6 -AM.1 25. -16.0

6 AR.o -60.A -;7.0 5Bnd -'o Z.1 la3.1 -50.1 -q8.8 34.0 -1A.2. A I4. -59. .9. A7. -R *4 9. -19 7. 34. p -118.017

C; 49.7 -4c;.8 -4ti.0 44+.1 0, 7 1 *- 7Z*7 -"-n*T -56.0 .1 . 1 . 3

10 1.4. 1.1.-. -2.4 1 1 1 1- . , . 61

.12*11 .1* 1 - 2- 1. P. * .-. 3 . -. 1 .. .1..

9-.0 *0 *0 -.0 *.0 -.0 *0 .0 .0 .0

1 ].7 1.4 -4.0 to . 1.6 -4.0 -2.3 2.2 .

2fl -*2 *7 .7 -*.~ .z .5 -5.0 , .7 *.0 ..3 .,S .0 .0 .17 * . .. 0 .o . ... -**

STRESS JT)UT ANAl YSTs

5072 60.1 *55,4 -50.2 56.3 -9.9 -.A 87.9 -49*1 -69.5 35.3 -18.3 13. 5060 67.0 -61.0 -7.5 5A,7 95 3.1 142.5 -44.7 -124.0 25.4 -18.5 19. 5063 81.9 -77.5 -72.4 74.4 -11.5 3.1 129. -67.0 -105.9 43.5 -23.3 23. 51?4 11.6 -10.6 *4.9 10.1 -6.7 .5 13.7 -12.2 -5.3 8.A -8.4 3. c;237 P.2 -1.9 .3 1,9 -2.5i .0 2.A o2.4 .0 1 .8 -2.8. 6059 -.1 .1 .2 .0 -.0 **2 -*2 .1 .2 .1 -. 0

6307.. .o 0 * .. .. .e 2 _ - 0

1i3 -. 7 C..' 45 -4. o?. -7........ 5.1 -4.4 .2.0 -1*

5o 6.7 6..8 -4. -. 1 *A.2 .4 6.3 7.5 -2.4 .9 -3.

O 1. 1.7 -4*0 -2.3 2.3 1*0 1*8 1.6 -4.0 -?.3 2.2 .

.STRESS Oiij ANALYSTS

. yes anAnlvt

) 0,0 6 IVAI. *N4c #1

TIER. PRTI4ARY + SFCONISAaY STFSS INTrASTTrz PEAK S1tFSS TI.rrNSTTTES c

L*R . R-H H-I L-H I-t1 iI-L

TNCSTI)F OilTATDFiw 0) T1I)E INSI'F OIJOi',1V OUTSIDE TNSTI). OUiTTIT I NII r

.3 T.7 -SR,? -4.7 %fi.? -4.1l 7,? 109.0 -56.7 ~9?.9 a2.l -1.0 28.

b 77.9 -7n.8 -61.6 S9. -14.0 11.3 115.0 -67.3 -q2.1 31 .3-2. A . . 7n.11 *71 .9 -. ?.9 ;9.? -?16.n 12.6 113.1 -71).6 -HJA.0 *2.7 . 1

I 1S A".T -63.' -47.3 4j%'.? -??.,n 1q.9 9S..) -IS. -64.2 311.0 -30.

TO 7.7 -60.9 -1210.-yR58 1.7 -9.4 -1I..0 1.2p -1.7 8 3o4 -e 4 -.

1491 .0 .0 .0 .0 .00 -** - .0 -*0 / .0 0 -.-.

. I?.7. 6 J .. 5 -1 .6. 131 0 2 5_* -3.5 -1. . 1..

fc.2 .0 .0 .0 - ,o .0 o. .0) .0

-.7 ., ..- , -* I' -l t . 4 --. .

STRFS5t f0JTFII AAi.YSJS

C;07? 86l.0 -7R.3 - .460.0 1-3. Fl. 117.3 -0. -A.1 34.7 -34, pR * 060 71.1 -66.8. -61.9 58.3 *II.? 8.4 147.4. -53.3 -121s.6 21.9 -1A.7 5063 97.9 -89. 15 -16,4 14.8 143.1 -85.3 -115.7 39.3 -?7.6

124 31.0 -19,7 -13.1 19.1 -)).A 14.7 c39.9 -36.7 -15.8 11.4 -24. c;37 1.5 -10.4 -1.R S.S -7.7 4.'. It.? -1..4 -5.I 4. -.7 8

6059 .4 -. 4 .3 .4 -. 7 *0 .e -. 5 .3 .3 -. 8

AT7 4 -. 4' . .3 -. 6 .0 .9 -. S 2 , AT3A -7.7 7.0 .6 -5.1 2 0.7 6.6 -4.3 3.1

9o 3.1 ~.0 .5 4. 5 -2.Q -1.6 4.1 -3.4 -. 4 4.7 1 2.? .6 -3.5 -1.6 1.3 1.0 0.5 . 9 -3.5 -1.6 1.0

STRESI )UTP. F ANALYSTS

9

I, ~~~~~4z I i %~t' 'f:

T.TFR PRIMARY * SrCnAfnARY STPFSS TNTFNSTTIF; PEAK STRYSS INTENSITIES

L-L -H H- L-R R-H H-L L

Mr0r flIJTSTflE INSInF 0ilTS1l) IN9I0F. n011"j1n0 INSTF 0TSIl)F INSIDE OUTSIr)E INjSll)E OITHI[

* 3 -P., A.5 71.S '4.4 -19.7 -11. -?.7 2.4 21.3 9.1 -18.6 6 .-1.3 ?.9 ??.1 9.5 -19.A -12.4 -3.p 2.8 P1.8 Q. -18.7 8 -3.7 3.3 ??*S 9.6 -lA.8 -I'lf.t -3. 3.? 2?.3 9.5 -lH.6 -12.f

S.-4.1 0 10.1 -1). -11.7 -4*1 3.I 23.(l 10.9 -1 .7 - 3, 30.8 1.0 10.3 -17.7 ~11.1 -4.1 2.5 21.7 10.6 -17.6 -17.

1?11 -7.1 1.8 1q.9 '.1 *-17.R -10.9 -2.. .1.4. 20.0 9.6 -17.A . rlI. 91 -.4 2.1 21.3 9.1 -la.@ -11.6 *?.4 2.1 71.3 9.5 -18.9 -11.1

STPFAs fliTPtil ANALYSIS

5l7* -4.7 4*0 23.0 9*4 -154 -13.5 -4,6 4.0 ?2.8 9.3 -)R.? -13 060 -P.6 2.2 21.0 9.3 -18.4 -11. 2. 2.2 20.9 9.? -1 i.4 -11 .9n63 -3. p. ?I. 9*4 -18.6 -1'? -3.1 P.7 21.6 9.3 -1n.5 -1 51?4 -5;.6 4.7 21.6 13.3* - 16. 0 -1.4 -2.?7 5.6 .18.7 12.3 -16.0 -7. S?17 -S.4 4.5 15. I. -10. -5. 4.O0- 4 *7w 4U?-,. 6(19. ?. .2 9-.7 1 5.9 -7) 1) . 7.1 6.3 -7.3 -1

6107 -1* 1* 9.7 4.6 -7.4 AI -. -. 4 10.0 6.6 -7. -6. o8 -1.4 R1.2 94 4.6 -8.0 -!5$ -1.A -. 8 9.7 6.6 -. 0 5.

A850 -121.1 12,2 5.5* -11.0 -110A -1.2 .1 17.2 5.5 -11.0-. . 1.1.. . 6 -1.3 -*. . P.? . .7 1.1 .6 -3.3 -1.2 2.2.

STRESS OJHIMiT ANALYSTS

s

1 . ... g V

) 0 0 6 iI 4 di').4 al '; T

TTFR PRIMARY SrrMImiiY sir'vs' INTF(IT Ir S PF.AK STPFSS iNTrNSITIFS

L H-L L- R- H-L

I NSI OE fillTSTI)F IN910I F 011TSiI N910 0US1' o Iw Ir v r OUT SIIJE INSIDE. oUTsiDF IN'l1). GI1TSTi

3 -. P. 4.6 -19.4 -14*1 24.A * -'i*0 4.4 -19.6 -14. 24.6 9.

-;. -2.9 -1R.R -14.0 24.7 .... 9. .* -5.1 5.0 -19.0 -14. 24.

. -6.6 . -1.3 -14.1 4. F 1 -6 4 75. -1P.6 -14.

15 -7.? 6.4 -17.1 -13.6 74.4 *.3 -7.? .3 .- 17.3 -13.7 ?.*4 7.

.30 -R..R 5.1 -14.2 -13.3 ?5.0 -4. * 8 -la.9 -13.1 25.1 *

1?1 -109 1*4 -?*i. -13.A ?3.P0. 11.9 -4.0 3.1 -19.9 -13.4 23.9 10.

.. 1 -4.4 3.9 -21.0 14.1 25.4 I. -4.4 3.9 21.0 -1'.? 25.4

4 -131 .4 -3.3 -1.4 1.4 .

1 l.Q .4 -3.3 -1.4 ~~~.4~ ~.s~-u. 'O Z

ZtS .2. g'7 q. 3. W iI 'b 0. . .. *. . . ...-.P-. *STRFSS OUjTPl T ANALYSIS

5072 -A.1 7.1 -17.7 -14.4 25. 3 7.0 -17.9 -14.4 5060 -4*7 4.2 -19.8 -14.? 24.6 10.0 -4.6 4.0 -2.0 -14.2 24.6 5063 -5.A 9.1 -19.0 -14.1 24.8 9.1 .-.. 6 4.9 -16.2 -12 26.1 9124 -Q*S 8.4 -16.4 -12.3 25.9 3.9 -9*3 2 -169 -10.9 A.

R37...*..7*8 -A.9 -10.6 ?7.8i 2.7 -A.(0 F.1 -19.9 -10.9 ?.0 6059 -4.5 3.9 -5*4 -4.4 9*8 .5 -5.01 3.3 -5.0 -37

Al07 -3.2 2.9 -4.8 -3.9 8.0 1.1 -3.5 1.4 -4.6 -2.4 8.0 63A8 -2.6 2.2 -5.2 -3.8 7.7 1.6 -2.8 .8 -4.9 -2.3 7.7

6850 -2.4 2.1 -31.6 -8.1 14.0 6.0 ' -7.4 2.1 -11.S -8.1 13.9 1 1.9 .4 -3.3 -1.4 1.4 .9 169 .4 -3.3 -1.4 1.4

STRFSS OA 1F LT ANALYSIS

e .. e

TTFR PRIMARY * SftONuay sTRFSS INTFNSTTIFS .pEASTRFS INTNSITIES

L R. 4. 0H - L

.H . . . -. R** .0H*L

3 *0 0 -. 0 . 0 . .

6 . .0 *0 -.* ... .....-.*..... _ *0 .. ... 0~ . 0* .00 9

P *..- .0 -. 0 -*0 .0. .0 -*00 .15~~6 .0 .. .*0..., * ... ^ -- - ---- ' . .* 1 4* .

30 *A *.5 -. 6 *S 3 - 0 -. 0

1-.3 * 3........*3 . *--.3 .... 3. .3 . .0

en .0 .0 -0 -*3 .1.2

1~ . - .1.1 _ * ."0* - . . . ..

50.0 .0.0. 5;174 ?*3

~f1? . . -0-. 0 .0 0 - .0 -0 -. .0

S.7 -. 0 -0 .0

c;0O63 .b0 .0 -*0 . -.0 0. 0* .0 -. -... * ?3 1.8 -?3 .8 1.-. 0 .5 -1.4 -4.5 .6 -. 1

91 P43 - 37.

0 .* 0* .0. *00

S737 Io, -1.5 -2.0 3.2 *2 1*7 11

6n9 -1.*7 1.1 2.1 3.3 -.3 **4*4 2.6 .4 2.1

0 7 -3.7 .) 4.2 4 -7.

-1.7 ?.5 4.1 4.2 -*4.7 -3R 3.3 4.1 4.6

4.1 6.4 *I * .- .2

S1. 1.1o3 1.1 62 -2 1.2

STRESS 0I11PIT ANALYSIS. .

g - .0 -. 0 -*0 .

~ ~ 4.5--*4--4.5 * .

.2.1 0. ..3.

.0.* .It26* . * -36.3 4 1 * *

-30334I . * 7

DETERMINATION OF MAXIMUM STRESS OSC 1522 INTENSITIES RANGES AND FATIGUE ANALYSIS

Segment 5: Page 5-16 gives a summary of thermal stress intensities

plusa--stress intensity for a 1000 psi pressure. The worst stress intensity

range for segment 5 would 3e full range of thermal stress from rapid depress

urization plus pressure variation of 1500 psi (pressure at start of rapid

depressurization) to 800 psi (pressure at time of reversal in thermal stress).

The smaller pressure range is chosen since the pressure stresses are small

and even the range of 2500 psi is less than the reversal in thermal stress.

This will be assumed to occur 40 times.

The next maormum range comes from mams thermal stress in the test

transient plus range in pressure of 2200-0 psi (2200 psi is pressure at time

of test).

The third range can be found using all the miscellaneous transients

excluding the rapid depressurisation and test transient. This last range

will be shown to be acceptable for infinite number of cycles.

Segment 8 is analyzed for essentially same conditions as segment 5.

Segment 23, the carbon steel segment, is analyzed differently since C

it has less radial gradient thermal effects and its stress picture is more

dependent on the temperature of the segment because of the bimetal weld.

Thus its highest stress intensity is derived from the range of its

highest thermal stress to 0 stress plus the range of pressure from 2500 psi

to 0. It is shown that all other ranges are essentially insignificant.

NOTE: This fatigue analysis includes thermal and mechanical discontinuity stresses only. For inclusion of stresses due to run and branch pipe motions, see Section "F".

21In Rev. I.

5-21

OMS-2'4;-1 .

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BABCOCK & WILCOX . REVISION

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BABCOCK &WILCOX REVISION

DF A nIN DATE______________-____-7_____Z______

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Documents

Design Report #7 B&W Contract No. FORINORMA7ON ONLY · composite transient curve developed for the cold leg fluid and the make-. -up fluid. Of primary importance was to select transients