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Two-Way-Coupling Method for Rapid Aerothermoelastic Analyses of Hypersonic Wings

Wan Zhiqiang Yi Nan Li Guoshu Yang Chao

南京航空航天大学学报（英文版）2018，Vol.35Issue(1)：135-145,11.

Two-Way-Coupling Method for Rapid Aerothermoelastic Analyses of Hypersonic Wings

Wan Zhiqiang ¹Yi Nan ²Li Guoshu ¹Yang Chao²

作者信息

1. School of Aeronautics Science and Engineering,Beihang University,Beijing 100191,P.R.China
2. Key Laboratory of Aircraft Advanced Design Technology(Behang University), Ministry of Industry and Information Technology,Beijing 100191,P.R.China
折叠

摘要

关键词

hypersonic/aerothermoelastic/two-way-coupling/aerodynamic heating/thermal deformation

Key words

hypersonic/aerothermoelastic/two-way-coupling/aerodynamic heating/thermal deformation

分类

航空航天

引用本文复制引用

Wan Zhiqiang,Yi Nan,Li Guoshu,Yang Chao..Two-Way-Coupling Method for Rapid Aerothermoelastic Analyses of Hypersonic Wings[J].南京航空航天大学学报（英文版）,2018,35(1):135-145,11.

基金项目

This work was supported partly by the National Natu-ral Science Foundation of China(Nos.11302011,11402013,11372023,11672018) （Nos.11302011,11402013,11372023,11672018）

the National Key Re-search and Development Program(No.2016YFB0200703) （No.2016YFB0200703）

and the Fundamental Research Funds for the Central Uni-versities(No.YWF-14-HKXY-006). （No.YWF-14-HKXY-006）

南京航空航天大学学报（英文版）

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ISSN：1005-1120

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