Thermal Post-buckling Analysis of Composite Laminate Plates
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 91 === Base on Von-Karman large deformation assumption and a simplified high order shear deformation plate theory, a 72 degree-of-freedom high precision high order triangular plate element is developed for the thermal post-buckling analysis of composite laminate pl...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2003
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| Online Access: | http://ndltd.ncl.edu.tw/handle/82134719921423370983 |