Free Vibration Analysis of Thermally Buckled Composite LaminatePlates
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 92 === Base on the von karman large deflection plate theory, a 54 degree-of-freedom high precision higher order triangular plate element is developed for free vibration of thermally buckled composite laminated plate. For buckled plate, the total response of the p...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Online Access: | http://ndltd.ncl.edu.tw/handle/99641483077415454522 |