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A Survey of Research on the Stability of Hydrostatically Loaded Shell Structures Conducted at the David Taylor Model BasinExperimental and theoretical studies have been carried out to investigate the stability of ring-stiffened cylinders and hemispherical shells under hydrostatic pressure. The use of accurately machined models has been found extremely valuable in improving the quality of experimental data, thereby permitting a more careful examination of theory. As a result, the effects of boundary conditions and other factors usually masked by the influence of structural imperfections have been clarified.

So far these studies have caused the investigators to regard classical small-deflection theory with increasing confidence.
Document ID
19630000973
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Thomas E. Reyno!ds
(David Taylor Model Basin Washington, DC, 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
63N10847
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
ROCKET NOZZLE
HYDROSTATIC PRESSURE
DEFLECTION
LOADING
SHELL STABILITY
BOUNDARY
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