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Composite-Material Point-Stress AnalysisPSANAL computes composite-laminate elastic and thermal properties and allowable load levels for any combination of applied membrane and bending loads occurring at a point. Basic linear orthotropic stress/ strain relationships and standard composite-laminate theory formulas are utilized.
Document ID
19810000245
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Spears, F., S. (Rockwell International Corp.)
Date Acquired
August 11, 2013
Publication Date
November 1, 1982
Publication Information
Publication: NASA Tech Briefs
Volume: 6
Issue: 2
ISSN: 0145-319X
Subject Category
Fabrication Technology
Report/Patent Number
MSC-18978
Accession Number
81B10245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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