Part 21 Report - 1995-078
ACCESSION #: 9502220192 Boeing Computer Services P.O. Box 24346 Seattle, WA 98124-0346 February 13, 1995 G-1151-RSO-95-079 Document Control Desk United States Nuclear Regulatory Commission Washington, D.C. 20555 BOEING 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, R. S. Orr Nuclear Administrator G-1151 M/S 7A-33 (206) 865-6248 Attachment(s): GTICES Program Report Form No. 95.02 Georgia Tech Computer Aided Structural Engineering Center Georgia Institute of Technology School of Civil & Environmental Engineering Atlanta, Georgia 30332-0355 USA 404-894-2260 February 3, 1995 404-894-8014 FAX Attention: Nuclear Administrator Boeing Computer Services P. O. Box 24346, M/S 7A-33 Seattle, Washington 98124-0346 RE: GT STRUDL Dear Sir or Madam: Enclosed please find a copy of the GTICES PROGRAM REPORT FORM No. 95.02 and a VENDOR ACKNOWLEDGEMENT FORM. Please sign and return the VENDOR ACKNOWLEDGEMENT FORM to acknowledge receipt of the GTICES Program Report. Thank you for reviewing the Program Report and for returning the Acknowledgement Form. Best regards, CASE Center Catherine Lee Configuration Control Manager CL/apw Enclosures 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. X MINOR Problem can be worked around or problem poses high frustration factor. INFORMATIVE Documentation error, program usage tip, user inconveniences. Date Problem Confirmed February 3, 1995 Date Notification Sent Computers All Operating System All Version All 91.01 and later Target Release for Correction 95.02 Manager, 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 DAMPING RATIOS command given immediately prior to the ASSEMBLE FOR DYNAMICS, DYNAMIC ANALYSIS EIGENVALUE, or DYNAMIC ANALYSIS MODE SUPERPOSITION commands will prevent the computation and assembly of the stiffness and mass damping matrices. This condition will furthermore result in the computation of 0.0 values for the modal damping ratios by the COMPUTE MODAL DAMPING command. The stiffness and mass damping ratios are computed and assembled as a result of damping factor values specified in any or all of the following commands: CONSTANTS, JOINT RELEASES, INERTIA OF JOINTS, DAMPING PROPORTIONAL. The following sequence of commands illustrates this situation: DAMPING RATIOS 0.05 10 ASSEMBLE FOR DYNAMICS $ No damping matrices assembled PERFORM EIGENVALUE ANALYSIS DYNAMIC PARAMETERS RESPONSE DAMPING INPUT 1.0 STIFFNESS 1.0 MASS 1.0 END COMPUTE MODAL DAMPING RATIOS $ 0 damping ratios computed Work-around: Position the DAMPING RATIOS command immediately before the COMPUTE MODAL DAMPING RATIOS command. Applicable sections of the User's Manual: Specification of Damping Properties -- Section 2.4.3.4, Volume 3 Rev. 2.2 *** END OF DOCUMENT ***
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Page Last Reviewed/Updated Wednesday, March 24, 2021