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Asymmetric Buckling of Clamped Shallow Spherical ShellsThe problem of buckling of clamped shallow spherical shells has recently been considered in several theoretical investigations. Buck-ling loads under uniform external pressure were obtained in these investigations which show a surprisingly good agreement with each other, but show a marked disagreement with available experimental values. In all previous studies it has been assumed that the shell deformations are rotationally symmetric. In this paper, the buckling problem is re-examined by introducing asymmetric modes of deformation. The approach is to superimpose small asymmetric deflections on finite axisymmetric deflections, and to show that the symmetric states of deformation are unstable over certain ranges of load and geometry parameter. Numerical results are obtained by means of a digital computer and are compared with previous theoretical and experimental results.
Document ID
19630000967
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hubertus J. Weinitschke
(Hughes Aircraft Co. Fullerton, CA, 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
63N10841
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
SPHERICAL SHELL
BUCKLING
SHELL STABILITY
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