Creep Buckling of Circular Cylindrical Shells in Pure Bending

Creep Buckling of Circular Cylindrical Shells in Pure Bending
Author: Stanford University. Department of Aeronautics and Astronautics
Publisher:
Total Pages: 62
Release: 1970
Genre: Buckling (Mechanics)
ISBN:

The two simultaneous nonlinear first-order differential equations characterizing the problems that were derived by the senior author in a paper in 1956 and were at that time solved for a few cases by numerical integration are solved here analytically with the aid of a few simplifying assumptions. The very simple formula derived in this manner is used to compute the critical times of a series of shells tested in the laboratory. It is found that the formula predicts somewhat larger values for the critical time than the experimental results. (Author).

NASA Memorandum

NASA Memorandum
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 384
Release: 1959
Genre: Aeronautics
ISBN: