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Stress, stability and vibration of complex, branched shells of revolutionA comprehensive computer program, designated BOSOR4, for analysis of the stress, stability, and vibration of segmented, ring-stiffened, branched shells of revolution and prismatic shells and panels is described. The program performs large-deflection axisymmetric stress analysis, small-deflection nonsymmetric stress analysis, modal vibration analysis with axisymmetric nonlinear prestress included, and buckling analysis with axisymmetric or nonsymmetric prestress. One of the main advantages of the code is the provision for realistic engineering details such as eccentric load paths, internal supports, arbitrary branching conditions, and a 'library' of wall constructions. The program is based on the finite-difference energy method, which is very rapidly convergent with increasing numbers of mesh points. The organization of the program is briefly described with the flow of calculations charted for each of the types of analysis. Overlay charts and core storage requirements are given for the CDC 6600, IBM 370/165, and UNIVAC 1108 versions of BOSOR4.
Document ID
19740044382
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bushnell, D.
(Lockheed Research Laboratories Palo Alto, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
March 1, 1974
Publication Information
Publication: Computers and Structures
Volume: 4
Subject Category
Computers
Accession Number
74A27132
Funding Number(s)
CONTRACT_GRANT: N00014-71-C-0002
CONTRACT_GRANT: NAS1-10929
Distribution Limits
Public
Copyright
Other

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