Thermally induced vibration of the flexible solar wing of the mast of space station
被引:0
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作者:
Kong, Xiang-Hong
论文数: 0引用数: 0
h-index: 0
机构:
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, ChinaCollege of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
Kong, Xiang-Hong
[1
]
Wang, Zhi-Jin
论文数: 0引用数: 0
h-index: 0
机构:
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, ChinaCollege of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
Wang, Zhi-Jin
[1
]
机构:
[1] College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
来源:
Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University
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2014年
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48卷
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08期
关键词:
Design and analysis - Displacement analysis - Equivalent temperature - Finite element analysis method - Linear dynamic analysis - Mast - Multiple disciplines - Thermally-induced vibrations;