| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 10295855 | Thin-Walled Structures | 2005 | 27 Pages |
Abstract
The exact buckling load is calculated by means of the computer code STAGS-A (Structural Analysis of General Shells[Almroth BO, Brogan FA, Meller E, Zele F, Petersen HT. Collapse analysis for shells of general shape, user's manual for STAGS-A computer code. Technical report AFFDL TR-71-8; 1973]) by adding a user written subroutine WALL, see Ref. [Goldfeld Y, Arbocz J. Buckling of laminated conical shells taking into account the variations of the stiffness coefficients. AIAA J 2004; 42(3):642-649]. The optimization problem is solved using response surface methodology.
Related Topics
Physical Sciences and Engineering
Engineering
Civil and Structural Engineering
Authors
Yiska Goldfeld, Johann Arbocz, Alan Rothwell,