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Computer program to compute buckling loads of simply supported anisotropic platesProgram handles several types of composites and several load conditions for each plate, both compressive or tensile membrane loads, and bending-stretching coupling via the concept of reduced bending rigidities. Vibration frequencies of homogeneous or layered anisotropic plates can be calculated by slightly modifying the program.
Document ID
19730000247
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Chamis, C. C.
Date Acquired
August 7, 2013
Publication Date
December 1, 1973
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-11961
Report Number: LEW-11961
Accession Number
73B10247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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