The instability improvement of the shape memory alloy composite plates subjected to in-plane parabolic temperature distribution
The designs of thin structure components of aerospace vehicles require the consideration of thermal buckling and post-buckling problems. Thermal buckling of the structures in the aerospace environment may occur due to non-uniformly distributed temperature field. A finite element method study on the...
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| 格式: | Article |
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Trans Tech Publication
2014
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| 在線閱讀: | http://eprints.utm.my/id/eprint/62974/ http://dx.doi.org/10.4028/www.scientific.net/AMM.554.32 |
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