ML20215B656
| ML20215B656 | |
| Person / Time | |
|---|---|
| Site: | Arkansas Nuclear  |
| Issue date: | 11/19/1983 |
| From: | Prescott K NUTECH ENGINEERS, INC. |
| To: | |
| Shared Package | |
| ML20215B645 | List: |
| References | |
| NUDOCS 8706170396 | |
| Download: ML20215B656 (18) | |
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COMPUTER PROGRAM VERIFICATION STARDYNE-'3'DEC01/82A H LEVEL NCSI CYBER 730 PROGRAMS STAR,.DYNREl, DYNRE2, DYNRE4, DYNRE5, DYNRE6 AND. POST j
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'l Prepared by:
Approved / Issued by:
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Prescott T. Q' Wenner Reviewed by:
a'a in n/n/ss V.
N. Anderson Date Issued.
l 8706170396 870605
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a COMPUTER PROGRAM VERIFICATION DOCUMENT j
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STARDYNF-3 DEC01/82A H Level j
Programs STAR,:DYNREl, DYNRE2, PROGRAM / VERSION:
DYNRE4, DYNRE5, DYNRE6, and POST FILE NO:
08.027.0200 j
The above-referencad program / version has been verified-inE accordance with QEP 3-5-and is valid for use in NUTECH's quality assurance-related work.
- <s %ss uNa Programmer Date Q L.W a n/As EngibNeringManager Date 1
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' QEP 3-5.3 Rev.0
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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, Category 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 version of STARDYNE (APR02/82).
The results obtained using both' versions are identical.
1 i
STARDYNE-3 1
d-8 3
f VERIFICATION' PROBLEM NUMBER 1 Program Used STAR Description of Problem Static analysisEof a 1/32 segment torus.model with card
'i image input. ' Inertia loads and hydrostatic pressure (concentrated forces) are applied.'. Stiffness matrix ir, f ormulated ' (TAPE 7), decomposed-(TAPE 9), and' solved for displacements and beam end loads (TAPE 4).
References APR02/82-DEC01/82A Job name AIIIFIP
.AIHQCMI Run rJate 12/05/82 11/02/83 Input Card image
- Card image
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- These card images were taken from TAPE 2 on CDC tape with VSN= pal 229.
STARDYNE-3 2
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u Ai VERIFICATION PROBLEM NUMBER 2 Program Used STAR Description of Problem Restart' static analysis of 1/32 segment torus model
'(verification problera number 1) with geometry input (TAPE 2)- and stiffnes matrix input (TAPE 9).
Internal pressure is applied using element pressure loads and
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concentrated forces.
References-APR02/82 DEC01/82A Job name AIIIFRI AIHQCLV Run date 12/05/82 11/02/83 Input-(TAPE 2, TAPE 9)
VSN=A00171 VSN=A00171 STARDYNE-3 3
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n VERIFICATION PROBLEM NUMBER 3-
.i Program'Used '
STAR-I l
Description o'f Probiem
' Restart staticnanalysis of,1/32 segment. torus.model for
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s-stress recovery with' geometry inputifrom verification o
' problem number 1- (TAPE 2).and ' displacements ' input s f rom
' verification:problemEnumber 2 (TAPE 4 input as Tl APE 14).
Element corner forces duelto internal pressurelloads'are computed for selected elements.
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'l References APR02/82 DEC01/82A-
' Job ~name '
'IIFSV.
AIHQCMN 11/02/83
.i Run date
'05/821.
~VSN=A00171 l
Input (TAPE 2)
EN=A0017L.
(TAPE 14)
/SN=A00172 VSN=A00172 1
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I STARDYNE-3
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. i VERIFICATION PROBLEM NUMBER 41 3
Program Used STAR Description of Problem Stiffness condensation of vent line-vent header i
intersection model with card image' input.
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References APR02/82 DEC01/82A Job name AIIIJXF' AIHQCMQ
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Run date, 12/06/82 11/02/83
-1 Input Card Image
-Card Image
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0 STARDYNE-3 5
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J VERIFICATION PROBLEM NUMBER 5.
t Program Used.
STAR Description of' Problem
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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.
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q References APR02/82 DEC01/82A'
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1 Job name AIIIFJX AIHQCMV Run date 12/05/82 11/02/83-Input.(TAPE 23) 1VSN=A00185 VSN=A00185 l
(TAPE 2, TAPE 9)
'VSN=A00168 LVSN=A00168 1
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VERIFICATION PROBLEM NUMBER =6 Program Used STAR Description of Problem Restart of 1/32 segment torus model-(verification-problem number 5) for additional modal stresses with geometry. input on TAPE 2 and eigenvectors input on TAPE 14.
'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
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STARDYNE-3 7
e VERIFICATION PROBLEM NUMBER 7 i
Program Used POST Description of Problem Postprocess 1/16 segment vent system model for combined displacements and beam end loads using results from TAPE 4 (input on TAPE 70).
l References APR02/82 DELG./82A j
Job name AIIIFKB AIHQCNB I
Run date 12/05/82 11/02/83 f
Input (TAPE 70)
USN=A00161 VSN=A00161 STARDYNE-3 8
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l VERIFICATICN PROBLEM NUMBER 8 j
i 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 l
white noise forcing function.
Transient output is computed for selected. nodes and elements, i
i References APR02/82 DEC01/82A Job name AIIIFWB AIHQCNH Run Date 12/05/82 11/03/83 Input (TAPE 4)
VSN=A00177 VSN=A00177 1
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STARDYNE-3 9
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VERIFICATION PROBLEM NUMBER 9 Program Used DYNRE2 Description of Problem Harmonic-analysis of 1/16 segment vent system model'with frequencies and eigenvectors input on TAPE 4..
C.O. vent 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 Job name AIIIFKE AIHQCNK Run date 12/05/82 11/02/83 Input (TAPE 4)
VSN=A00161 VSN=A00161 4
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VERIFICATION PROBLEM NUMBER 10-1 Program Used.
DYNRE4 Description of Problem s
Response spectra analysis of 360 degree vent system j
model' with frequencies and eigenvectors input on 1
TAPE 4.
Earthquake spectra is applied in three directions and combined by SRSS.
Closely spaced modes are combined using the 10 percent rule..
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References APR02/82 DEC01/82A i
.I Job name AIIIFKF AIHQCNO Run date 12/05/82 11/03/83 Input (TAPE 4)
VSN=A00186 VSN=A00186 1
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1 STARDYNE-3 11
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.c VERIFICATION PROBLEM' NUMBER 11-Program-Used' DYNRES-Description of Problem" Generate response-spectra from displacement' time history
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-input-on TAPE 54.
References APR02/82 DEC01/82A Job name AIIIFTA AIHQCNR Run date 12/05/82 11/03/83.
Input (TAPE 54)
VSN=A00187 VSN=A00187 l
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STARDYNE 12
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l-J VERIFICATION PROBLEM NUMBER 12 Program Used DYNhE6 s
Description'of Problem Dynamic analysis.of a simplified model1of an in-vessel storage rack with nonlinear gapEelements where the
. structure rests against:the vessel wall.
An acceleration time history base acceleration load is applied in all three' global-directions.
I References APR01/82-DEC01/82A Job name AIHQJOE AIHOGVT-Run date 6/09/83 11/03/83 Input (TAPE 7).
VSN=A02072 VSN=A02072 i
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STARDYNE-3 13
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i ENCLOSURE 5 EXCERPT FROM TMRSAP VERIFICATION REPORT 4
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'As ENGINEERING SERVICES j
130 SECOND AVENUE j
WALTHAM, MASSACHUSETTS 02254 fl N,h[,lf y' {
'5") 8' '8 5 "In i 2usca
'h 'If lf o ;9,qg-April 25, 1986 A600 En nN - gkm/t%nicatR E llCHT CD' Mr. Morris Byram Arkansas Public Power
~P.O. Box 551 FCB-9 l
Little Rock, Arkansas, 72203 j
Subject:
TMR-SAP Verification
Dear Sir:
Per your telecon with Mr. Lenin Semprucci, Principal Engineering for Teledyne Engineering Services, I have enclosed a copy of the first pages of the Verification Manual for our TMR SAP Computer Program. I hope this will be sufficient enough to assure you of"the verification of this program.
If you have any questions or need any futher information concerning this program please contact me at your convenience.
Yours truly, TELEDYNE ENGINEERI.F 'ERVICES Donald Messinger Manager, Quality Assurance s
DM:mid attachment j
I ENGINEERS AND METALLURGISTS