Influence of modelling and solution methods on the FE-simulation of the post-buckling behaviour of stiffened aircraft fuselage panels
Author(s): |
P. Linde
A. Schulz W. Rust |
---|---|
Medium: | journal article |
Language(s): | English |
Published in: | Composite Structures, May 2006, n. 2, v. 73 |
Page(s): | 229-236 |
DOI: | 10.1016/j.compstruct.2005.11.048 |
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10461720 - Published on:
25/10/2020 - Last updated on:
25/10/2020