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Flight Dynamic Analysis of Hypersonic Vehicle Considering Liquid-Solid Coupling

Xu Xiaodong Huang Yimin Cai Xiaobin

南京航空航天大学学报（英文版）2015，Vol.32Issue(1)：81-88,8.

Flight Dynamic Analysis of Hypersonic Vehicle Considering Liquid-Solid Coupling

Xu Xiaodong ¹Huang Yimin ²Cai Xiaobin¹

作者信息

1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautic,Nanjing 210016, P.R.China
2. Research Institute of UAV, Nanjing University of Aeronautics and Astronautic,Nanjing 210016, P.R.China
折叠

摘要

关键词

hypersonic vehicles/liquid propellant sloshing/coupling model/structure vibration

Key words

hypersonic vehicles/liquid propellant sloshing/coupling model/structure vibration

分类

航空航天

引用本文复制引用

Xu Xiaodong,Huang Yimin,Cai Xiaobin..Flight Dynamic Analysis of Hypersonic Vehicle Considering Liquid-Solid Coupling[J].南京航空航天大学学报（英文版）,2015,32(1):81-88,8.

基金项目

This work was supported by the Fundamental Research Funds for the Central Universities (No.NS2015097). （No.NS2015097）

南京航空航天大学学报（英文版）

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ISSN：1005-1120

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