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Accession Number:
AD0781329
Title:
The Effect of Geometric Nonlinearities on the Creep Buckling of Axially Compressed Circular Cylindrical Shells.
Descriptive Note:
Technical rept.,
Corporate Author:
STANFORD UNIV CALIF DEPT OF AERONAUTICS AND ASTRONAUTICS
Report Date:
1974-04-01
Pagination or Media Count:
9.0
Abstract:
A correction is given to the small-displacement theory of the axisymmetric creep buckling of axially compressed circular cylindrical shells. The correction takes into account the possibility of a non-axisymmetric elastic snap through in agreement with Koiters theory after a sufficient amount of axisymmetric permanent deformation has developed in consequence of creep. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE