NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Buckling of Initially Imperfect Axially Compressed Cylindrical ShellsThe effects of imperfections on the buckling strength of pressurized cylinders under axial compression are studied. The imperfection factor is considered in the finite-deflection compatibility equation, as well as in the equilibrium equation. A new relation to express the imperfection as an explicit exponential function of pressure and radius thickness ratio is proposed. A method for finding the exponential function is described, and the solution for the
critical stress is found in a fairly simple form. The relation of decrease of stability with respect to magnitude of imperfections if found.
Document ID
19630000947
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
S. Y. Lu
(University of Florida Gainesville, Florida, United States)
William A. Nash
(University of Florida Gainesville, Florida, 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
63N10821
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
CYLINDRICAL SHELL
BUCKLING
AXIAL COMPRESSION
No Preview Available