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The sensitivity of buckling of axially compressed fiber-reinforced cylindrical shells to small geometric imperfectionsBuckling sensitivity of axially compressed fiber reinforced cylindrical shells to small geometric imperfections
Document ID
19690030859
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Card, M. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1969
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-61914
Report Number: NASA-TM-X-61914
Accession Number
69N40244
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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