Thermally induced vibration of the flexible solar wing of the mast of space station

被引：0

作者：

Kong, Xiang-Hong ^{[1
]}

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 | 2014年 / 48卷 / 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;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：1103 / 1108