ML20215B568
| ML20215B568 | |
| Person / Time | |
|---|---|
| Site: | Arkansas Nuclear  |
| Issue date: | 11/19/1983 |
| From: | Anderson V, Prescott K, Wenner T NUTECH ENGINEERS, INC. |
| To: | |
| Shared Package | |
| ML20215B273 | List: |
| References | |
| NUDOCS 8706170369 | |
| Download: ML20215B568 (15) | |
Text
{{#Wiki_filter:,. - e, e.. e- 'l ~ .o. i File: 08.027.0200 i j COMPUTER PROGRAM VERIFICATION STARDYNE-3 DEC01/82A H LEVEL NCSI CYBER 730 PROGRAMS STAR, DYNREl, DYNRE2, DYNRE4, DYNRES, DYNRE6 AND POST I 1 Prepared by: Approved / Issued by:
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' ' ~ ' K. S. Prescott T. W. Wenner Reviewed by: ll!d!b3 [ Mg V. N. Anderson Date Issued l 0706170369 870612 PDR ADOCK 05000313 i PDR p l I
ef - 7 d l. COMPUTER PROGRAM VERIFICATION DOCUMENT STARDYNE-3 DEC01/82A H Level Programs STAR, DYNREl,,DYNRE2, PROGRAM / VERSION: DYNRE4, DYNRES, DYNRE6, and POST FILE'NO: 08.027.0200 The above-referenced program / version has~been verified in accordance with QEP 3-5 and is valid for use in NUTECH's. quality j ] assurance-related work. SC6 I H f3 f O fb. Programmer' Date .hM ll[19 f63 f EngibNeringManager Date Subsequent revisions of this program shall be verified and documented on the following computer program revision control table. DATE __ REV/VER-NO. VERIFIED PROGRAMMER ENGINEERING MGR l i i j l QEP 3-5.3 Rev.0
-ec ) INTRODUCTION STARDYNE programs STAR, DYNREl, DYNRE2, DYNRE4, DYNRES, DYNRE6 and POST have been installed on the OPTICOM Corporation CYBER 730 computer installation. STARDYNE is a Category 1 program; .however,fCategory 2 verification is provided by NUTECH Engineers in absence of verification by OPTICOM. Twelve verification problems were run and compared to the results of the previous a version of STARDYNE ' ( APR02/02). The results obtained.using both versions are identical. ~1 i l l STARDYNE-3 1
/ ~~. VERIFICATION-PROBLEM NUMBER 1 Program-Used. ' STAR Description"of Problem 3 ~ i . Static analysis of.a'l/32. segment torus'model with card image input.:. Inertia loads and1 hydrostatic pressure (concentrated forces) are applied.. Stiffness matrix'is 1 formulated L (TAPE 7), decomposed (TAPE 9), and solved for. j displacements and beam end loads'(TAPE 4). l 4 References-APR02/82' DEC01/82A-
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Job name AIIIFIP AIHL> t'I J Run date 12/05/82 '11/02/83 j Input-Card image
- Card image *
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- These card images were taken from TAPE 2 on CDC tape with VSN=PA1229.
STARDYNE-3 2
l4 t . ;c., .l 1 .'). ~ VERIFICATION PROBLEM NUMBER 2 Program Used STAR q Description of Problem ) I ~ Restart ' static ~ analysis' of 1/32 ' segment torus model:- -{ d (verification problem number.1) Lwith geometry. input: (TAPE 2)' and stiffnes. matrix input-(TAPE 9).. Internal' . pressure is applied using' element. pressure 11oads and E j concentrated forces. J . i References APR02/82- -DEC01/82A l (, Job.name: AIIIFRI 'AIHQCLV. l ' Run. dete' 12/05/82 11/02/83 j l rIn;!.r. (TAPE 2, TAPE 9) VSN=A00171 VSN=A00171 h h - l l a i 1 1 3 STARDYNE-3
{m zl J. : E L s VERIFICATION PROBLEM NUMBER 3-o Program Used STAR Description ~of Problem Restart static analysis of 1/32 segment torus model for stress recovery with. geometry input'from verification problem. number 1 (TAPE 2) and displacements input from ... ~ verification problem number 2 (TAPE 4 input.as: TAPE 14). I Element corner-forces due to internal pressure loads.are ' computed for selected elements. 1 ' References APR02/82 'DEC01/82A . Job name-AIIIFSV AIHQCMN RunLdate 12/05/82 11/02/83 Input - (TAPE 2) VSN=A00171 VSN=A00171. (TAPE 14) VSN=A00172 VSN=A00172 h i ~STARDYNE-3 4 l
l L e.. VERIFICATION PROBLEM NUMBER 4-1 I-Program Used ' STAR Description of Problem l Stiffness condensat' ion of. vent line-vent header intersect. ion model with card image input. References APR02/82 DEC01/82A l Job name AIIIJXF AIHQCMQ Run date 12/06/82 11/02/83 Input Card Image Card Image ) .1 1 l ~! 1 l f STARDYNE-3 5
VERIFICATION PROBLEM NUMBER 5 Program Used ' STAR Description of Problem Frequency analysis (LANCZOS) of 1/32 torus model with. card image geometry input, consistent mass matrix input on' TAPE 23, and stiffness matrix input'on TAPE 9. t 1 References APR02/82 DEC01/82A Job name' .AIIIFJX AIHQCMV Run date 12/05/82 11/02/83 ' Input (TAPE 23) VSN=A00185-VSN=A00185 .(TAPE 2, TAPE 9) VSN=A00168 VSN=A00168 1 i ~ k 1 i ) 4 l STARDYNE-3 6 l
o :: j VERIFICATION' PROBLEM-NUMBER 6 .j Program Used, STAR Description of Problem-Restart of 1/32 segment torus model (verification i problem number 5) for additional modal stresses with i geometry input on TAPE 2 and eigenvectors input on TAPE 14. j I References APR02/82 DEC01/82A Job name AIIIFKA AIHQCMY Run date 12/05/82 -11/02/83 Input (TAPE 2, TAPE 14) VSN=A00168 VSN=A00168 l s l 4 4 STARDYNE-3 7
,l' 4 F VERIFICATION-PROBLEM NUMBER 7 Program Used POS* Description of' Problem n l Postprocess'l/16 segment vent system model for combined i displacements and beam end loads using results from TAPE 4.(inputHon TAPE 70). References APR02/82 DEC01/82A Job name AIIIFKB AIHQCNB Run'date 12/05/82 11/02/83 LInput (TAPE 70) USN=A00161 .VSN=A00161 l b l STARDYNE-3 8
1.", VERIFICATION PROBLEM NUMBER 8 Program Used' DYNREl Description of Problem ' Transient analysis of 1/32 segment: torus'model with frequencies and eigenvectors input on TAPE 4. Single valve SRV pressure applied (concentrated forces). with. I white noise forcing function... Transient output is computed for selected. nodes and elements. .\\ References APR02/82 .DEC01/82A Job name .AIIIFWB AIHQCNH Run'Date-12/05/82-11/03/83 Input (TAPE 4) VSN=A00177 VSNr.A00177 1 ) 1 STAROYNE-3 9 9
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VERIFICATION PROBLEM NUMBER 9 l Prograta Used DYNRE2 d Description of Problem 3 i ' Harmonic analysis of 1/16 segment vent system model with ) frequencies and eigenvectors input on. TAPE 4. .C.O. vent j system. pressure'is applied (concentrated forces) over a specified; frequency range. Frequency sweep is performed- 'for selected degrees-of-freedom. I References APRJ02/82 DEC01/82A i 1 L L Job name AIIIFKE AIHQCNK Run date 12/05/82 11/02/83 - ) Input'(TAPE 4) -VSN=A00161 VSN=A00161 l 1 ^1 ~1 l l: i STARDYNE-3 10
1 'j ': .c. VERIFICATION' PROBLEM NUMBER 10 Program-Used DYNRE4 Description of Problem i-Response spectra analysis of 360 degree vent system model with frequencies and eigenvectors input on TAPE 4. Earthquake spectra is applied in three 1 directions and combined by,SRSS. Closely spaced modes are combined using the.10 percent rule. References APR02/82 DEC01/82A Job name AIIIFKF AIHQCNO Run date 12/05/82 11/03/83 Input (TAPE 4) VSN=A00186 VSN=A00186 4 s STARDYNE-3 11
f. R .g R VERIFICATION' PROBLEM NUMBER 11 Program Used DYNRE5 i' t ~ ) Description of Problem i Generate' response spectra from displacement time history 3 h input on TAPE 54. l i References APR02/82-DEC01/82A Job name AIIIFTA AIHQCNR ~ .Run date 12/05/82 11/03/83 Input'(TAPE 54) VSN=A00187 VSN=A00187 { i ~ i [ b 3 STARDYNE-3 12 e 4
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. C. 4 VERIFICATION PROBLEM NUMBER 12 Program Used -DYNRE6 Description of' Problem } Dynamic' analysis of a simplified.model.of an in-vessel J storage rack.with nonlinear gap elements where.the structure. rests against the vessel wall. An. acceleration time history base acceleration-load is applied in all three-global directions. l 1 ' l i References APR01/82 DEC01/82A t Job'name-AIHQJOE AIHQGVT Run date 6/09/83 11/03/83 Input (TAPE 7) VSN=A02072 .VSN=A02072 i
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