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Experiments to determine the strength of filament-wound cylinders loaded in axial compressionCompressive strength of glass-epoxy multilayer filament wound cylinders loaded in axial compression
Document ID
19660023039
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Card, M. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3522
Report Number: NASA-TN-D-3522
Accession Number
66N32329
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FILAMENT WINDING
CYLINDRICAL SHELL
AXIAL COMPRESSION
COMPRESSION LOADING

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