Thermally induced vibration analysis of thin composite plate based on hybrid element model

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Chang, Xiaoquan [1 ]
Luo, Zhiwei [1 ]
Zheng, Gangtie [1 ]
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[1] School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China
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页码:18 / 24
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