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The Buckling of Circular Cylindrical Shells Subject to Axial ImpactEarly experimental results on the buckling of circular cylindrical shells subject to axial impact are described. A hypothesis for the mechanism of buckling which was based on these experiments is described. The results of further experiments which were designed to test predictions from the hypothesis and which appear to verify it in several aspects are then described.
Document ID
19630000961
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Anthony P. Coppa (General Electric (United States) Boston, Massachusetts, United States)
Date Acquired
August 1, 2013
Publication Date
October 24, 1962
Publication Information
Publication: Collected Papers on Stability of Shell Structures - 1962
Publisher: National Aeronautics and Space Administration
Volume: Technical Note: D-1510
Issue Publication Date: December 1, 1962
Subject Category
Thermodynamics And Combustion
Meeting Information
Meeting: NASA Symposium on Instability of Shell Structures
Location: Hampton, VA
Country: US
Start Date: October 24, 1962
End Date: October 25, 1962
Sponsors: Langley Research Center
Accession Number
63N10835
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
IMPACT
CIRCULAR CYLINDER
SHELL STABILITY
CIRCULAR SHELL
BUCKLING
CYLINDRICAL SHELL

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