Part 21 Report - 1997-551
ACCESSION #: 9709040119
Information & Support Services
P.O. Box 3707
Seattle, WA 98124-2207
August 27, 1997
G-1151-SJA-97-395
Document Control Desk
United States Nuclear Regulatory Commission
Washington, D.C. 20555
Reference: a) Boeing Letter G-1151-RSO-92-365 dated August 31,
1992; R. S. Orr to the NRC Operations Center
b) NRC Letter Docket No. 99901227 dated August 12, 1992;
L. J. Norrholm to R. S. Orr; Subject: Response to 10
CFR 21 Inquiry
Dear Sir or Madam:
In accordance with the reference correspondence and 10 CFR 21, Boeing is
sending the NRC the attached error notice(s) received from our former
software suppliers. Because of unknown current addresses, the following
former customers were not notified:
Reactor Controls, Inc.
Echo Energy Consultants, Inc.
Nuclear Applications and Systems Analysis Company (Japan)
Nuclear Power Services
Error notices have been sent to our other former customers.
Very truly yours,
Sandra J. Andrews
Nuclear Administrator
Phone: (206) 865-6248
FAX: (206) 865-4851
Mail Stop: 7A-33, or
e-mail: Sandra.Andrews@PSS.Boeing.com
Enclosure(s): GTSTRUDL Program Report Form 97.07
Georgia Institute
of Technology GTSTRUDL [Registered Copy]
AUG 26 1997
August 19, 1997
Attention: Nuclear Administrator
Boeing Information & Support Services
P.O. Box 24346, M/S 7A-33
Seattle, Washington 98124-0346
RE: GT STRUDL
Dear Sir or Madam:
Enclosed please find copies of GTSTRUDL PROGRAM REPORT FORM 97.07 and a
GTSTRUDL QA CUSTOMER ACKNOWLEDGEMENT FORM. Please sign and return the
GTSTRUDL QA CUSTOMER ACKNOWLEDGEMENT FORM to acknowledge receipt of the
GTSTRUDL Program Report.
Thank you for reviewing the Program Report and for returning the
Acknowledgement Form.
Best regards,
CASE Center
David C. Key
Configuration Control Manager
Enclosures
Computer Aided Structural Engineering Center Phone: (404) 894-2260
School of Civil & Environmental Engineering Fax: (404) 894-8014
Atlanta, Georgia 30332-0355 USA casec@ce.gatech.edu
A Unit of the University System of Georgia
GTSTRUDL Program Report Form
GPRF No.:
DATE:
FROM: Computer-Aided Structural Engineering Center
Georgia Institute of Technology
Atlanta, Georgia 30332-0355
SEVERITY LEVEL:
_ URGENT Problem results in incorrect answers which may not be
apparent or job aborts and cannot be recovered within the
session or job.
_ SERIOUS Problem results in incorrect answers which are obvious or
problem prevents completion of a particular user's task.
_ MINOR Problem can be worked around or problem poses high
frustration factor.
_ INFORMATIVE Documentation error, program usage tip, user
inconveniences.
Date Problem Confirmed August 18, 1997
Date Notification Sent
Computers PC
Operating System DOS, Windows NT, Windows 95
Version All versions up to and including 97.01
Target Release for Correction 98.01
Mgr. ASD
Signature Title
R & D Division
Michael H. Swanger
Typed or Printed Name Date of Signature
Signature Title
Professional Services Division
Typed or Printed Name Date of Signature
Rev. 2.2
GTSTRUDL Program Report Form
(Continued)
GPRF No.:
DATE:
DESCRIPTION:
The NONLINEAR ANALYSIS CONTINUE command will abort if a new load is
created or a previously inactive load is newly activated prior to
execution. This is not a valid operation. The NONLINEAR ANALYSIS
CONTINUE
command expects results to be available for the currently active load
from
previous NONLINEAR ANALYSIS or NONLINEAR ANALYSIS CONTINUE commands. An
example of the command sequence that causes the abort follows:
UNITS KIPS INCHES
LOADING 1
JOINT LOADS
1 TO 10 FORCE Y -10.0
MAXIMUM NUMBER OF CYCLES 10
CONVERGENCE TOLERANCE DISPLACEMENT 0.001
NONLINEAR ANALYSIS
$
$ Loading 2 is a new load with no results from a previous
analysis.
$ NONLINEAR ANALYSIS CONTINUE expects results to be available.
$
LOAD 2
JOINT LOADS
1 TO 10 FORCE Y -20.0
LOAD LIST 2
NONLINEAR ANALYSIS CONTINUE
The correct way to do this is shown below:
UNITS KIPS INCHES
LOADING 1
JOINT LOADS
1 TO 10 FORCE Y -10.0
Rev. 2.2
MAXIMUM NUMBER OF CYCLES 10
CONVERGENCE TOLERANCE DISPLACEMENT 0.001
NONLINEAR ANALYSIS
$
$ The total joint loads applied to joints 1 to 10 is -20.0 kips
in the global Y direction.
$ Use CHANGES and ADDITIONS modes to add an additional -10.0
kips to
$ loading 1.
$
CHANGES
LOAD 2
ADDITIONS
JOINT LOADS
1 TO 10 FORCE Y -10.0
LOAD LIST 1
NONLINEAR ANALYSIS CONTINUE
Rev. 2.2
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