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Computer program for numerical analysis of stiffened shells of revolutionPrograms, using Love-Reissner first-order shell theory, can analyze orthotropic thin shells of revolution subjected to unsymmetric distributed loading or concentrated line loads and thermal strains. They can perform stability or vibration analysis of thin shells of revolution subjected to axisymmetric distributed loading or concentrated line loads and thermal strains.
Document ID
19750000094
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Key, J. (Grumman Aerospace Co.)
Svalbonas, V.
Date Acquired
August 8, 2013
Publication Date
June 1, 1975
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-23027
Report Number: MFS-23027
Accession Number
75B10094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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