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User document for computer programs for ring-stiffened shells of revolutionA user manual and related program documentation is presented for six compatible computer programs for structural analysis of axisymmetric shell structures. The programs apply to a common structural model but analyze different modes of structural response. In particular, they are: (1) Linear static response under asymmetric loads; (2) Buckling of linear states under asymmetric loads; (3) Nonlinear static response under axisymmetric loads; (4) Buckling nonlinear states under axisymmetric (5) Imperfection sensitivity of buckling modes under axisymmetric loads; and (6) Vibrations about nonlinear states under axisymmetric loads. These programs treat branched shells of revolution with an arbitrary arrangement of a large number of open branches but with at most one closed branch.
Document ID
19730010203
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cohen, G. A.
(Structures Research Associates Laguna Beach, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-2086
Report Number: NASA-CR-2086
Accession Number
73N18930
Funding Number(s)
PROJECT: RTOP 501-22-01-02
CONTRACT_GRANT: NAS1-10091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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