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On The Instability of Orthotropic CylindersPreliminary results from experimental investigations on the buckling strength of rlng-and-strlnger stiffened aluminum cylinders and filament-wound glass-epoxy cylinders are compared with instability calculations based on small-deflection orthotropic cylinder theory. Correlation
between experiment and calculation was reasonably good for the glass-epoxy cylinders; however, correlation for the ring-and-stringer stiffened cylinders cam be achieved only when some of the basic wall stlffnesses for stiffened cylinders with buckled skin can be better defined. In particular, the wall shear stiffness and the wall bending stiffness in the circumferential direction need better definition.
Document ID
19630000956
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Michael F. Card
(Langley Research Center Hampton, Virginia, United States)
James P. Peterson
(Langley Research Center Hampton, Virginia, 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
63N10830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ORTHOTROPIC CYLINDER
BUCKLING
SHELL STABILITY
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