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THE EFFECT OF INITIAL IMPERFECTIONS ON THE BUCKLING STRESS OF CYLINDRICAL SHELLSEffect of axially symmetrical initial imperfection on buckling load of circular cylindrical shell under axial compression loading
Document ID
19630008791
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Babcock, C. D. (California Inst. of Tech. Pasadena, CA, United States)
Sechler, E. E. (California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1963
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-2005
Report Number: NASA-TN-D-2005
Accession Number
63N18668
Funding Number(s)
CONTRACT_GRANT: NSG-18-59
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CYLINDRICAL SHELL
COMPRESSION LOADING
AXIAL COMPRESSION
CIRCULAR SHELL
BUCKLING

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