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Instability Analysis of Cylindrical Shells Under Hydrostatic PressureTo determine the elastic buckling pressure of simply supported cylindrical shells subjected to lateral end axial hydrostatic forces, various versions of linear bending theories have been employed in the past. For certain shell dimensions, however the expressions commonly
used may yield substantially differing results. In what follows, recent work on this problem by A. E. Armenakas and the writer is briefly reviewed. This work consisted primarily in employing a general
bending theory of circular cylindrical shells under the influence of initial stress, developed earlier by the same authors, to re-examine the problem mentioned, and compare the results with those of previous investigations. The outcome was the establishment of a simple but accurate expression for the buckling pressure applicable to a wide range of shell dimensions.
Document ID
19630000951
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
George Herrmann
(Northwestern University Evanston, Illinois, 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
63N10825
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
CYLINDRICAL SHELL
SHELL STABILITY
HYDROSTATIC PRESSURE
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