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Buckling of Orthotropic and Stiffened Conical ShellsDonnell type stability equations for thin circular orthotropic conical shells are presented and solved for external pressure, axial compression and combined loading. The solution is likewise applied to stiffened conical shells. Correlation with equivalent cylindrical shells yields a simple approximate stability analysis for orthotropic or ring-stiffened conical shells under hydrostatic pressure. The general instability of stiffened conical shells under hydrostatic pressure is also analysed by a more accurate approach. Preliminary experimental results for buckling of ring-stiffened conical shells under hydrostatic pressure are presented and discussed.
Document ID
19630000966
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Josef Singe
(Technion – Israel Institute of Technology Haifa, Israel)
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
63N10840
Funding Number(s)
CONTRACT_GRANT: AF-EOAR-62-61
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
CONICAL SHELL
SHELL STABILITY
BUCKLING
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