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Enhancements to the STAGS computer codeThe power of the STAGS family of programs was greatly enhanced. Members of the family include STAGS-C1 and RRSYS. As a result of improvements implemented, it is now possible to address the full collapse of a structural system, up to and beyond critical points where its resistance to the applied loads vanishes or suddenly changes. This also includes the important class of problems where a multiplicity of solutions exists at a given point (bifurcation), and where until now no solution could be obtained along any alternate (secondary) load path with any standard production finite element code.
Document ID
19870002586
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rankin, C. C.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Stehlin, P.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Brogan, F. A.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1986
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
LMSC-D060755
NAS 1.26:4000
NASA-CR-4000
Report Number: LMSC-D060755
Report Number: NAS 1.26:4000
Report Number: NASA-CR-4000
Accession Number
87N12019
Funding Number(s)
PROJECT: RTOP 505-63-31-01
CONTRACT_GRANT: NAS1-16723
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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