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Axisymmetric Snap Buckling of Conical ShellsThe authors give a brief account of some of their recent analytical and numerical studies of cone buckling. limiting the discussion to axisymmetric deformations.

Pertinent numerical results for the relaxation buckling of full cones subjected to uniform external pressure and Belleville springs deformed by axial edge loads are presented. In addition. bifurcation buckling problems are discussed. For a specific case. the existence of Friedrichs' intermediate buckling load, P(m). as applied to cones. is established. Upper and lower bounds for its value are given.
Document ID
19630000965
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Malcolm Newman
(Republic Aviation Corporation New York, NY, United States)
Edward L. Reiss
(New York University New York, New York, 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
63N10839
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
LOADING
SHELL STABILITY
BUCKLING
CONICAL SHELL
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