Creep Buckling of Circular Cylindrical Shells in Pure Bending
Download or Read eBook Creep Buckling of Circular Cylindrical Shells in Pure Bending PDF written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on 1970 with total page 62 pages. Available in PDF, EPUB and Kindle.
Author | : Stanford University. Department of Aeronautics and Astronautics |
Publisher | : |
Total Pages | : 62 |
Release | : 1970 |
ISBN-10 | : STANFORD:36105046320979 |
ISBN-13 | : |
Rating | : 4/5 (79 Downloads) |
Book Synopsis Creep Buckling of Circular Cylindrical Shells in Pure Bending by : Stanford University. Department of Aeronautics and Astronautics
Book excerpt: 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).