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Buckling of Layered Orthotropic and Sandwich Cylindrical Shells in Axial CompressionResults of modifications of large-deflection theory for isotropic materials to shells constructed of orthotropic layers and sandwich are presented. Experimental evaluation of the buckling of a rather extensive series of plywood cylinders and of a few curved panels of sandwich construction shows reasonably good agreement with buckling predicted by theory.
Document ID
19630000958
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Edward W. Kuenzi (US Forest Service Washington D.C., District of Columbia, 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
63N10832
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BUCKLING
ORTHOTROPIC SHELL
AXIAL COMPRESSION
SHELL STABILITY

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