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Thermal buckling analysis for stiffened orthotropic cylindrical shellsStructural analysis of thermal buckling of orthotropic, multilayered, stiffened cylindrical shell using finite differences and determinant plotting or modal iteration
Document ID
19710014258
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Card, M. F. (NASA Langley Research Center Hampton, VA, United States)
Chang, L. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1971
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-6332
L-7021
Report Number: NASA-TN-D-6332
Report Number: L-7021
Accession Number
71N23734
Funding Number(s)
CONTRACT_GRANT: 722-02-10-02-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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