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The buckling strength of filament-wound cylinders under axial compressionBuckling strengths of axially compressed filament wound cylinders determined by linear anisotropic shell theory
Document ID
19650019355
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Feldman, A. (Martin Co. Denver, CO, United States)
Stang, D. A. (Martin Co. Denver, CO, United States)
Tasi, J. (Martin Co. Denver, CO, United States)
Date Acquired
August 2, 2013
Publication Date
July 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-266
Report Number: NASA-CR-266
Accession Number
65N28956
Funding Number(s)
CONTRACT_GRANT: NASW-912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CYLINDRICAL SHELL
COMPRESSION BUCKLING
FILAMENT WINDING

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