Numerical studies on the thermal-fluid-structure coupling analysis method of hypersonic flight vehicle

•An elastic hypersonic configuration via delta wings with large sweep angle was designed.•A thermal-fluid-structure coupling method is proposed to analyze the thermal conditions of hypersonic vehicle.•Thermal dynamics and thermal flutter stability were presented for the present hypersonic aircraft....

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Bibliographic Details
Published inThermal science and engineering progress Vol. 40; p. 101792
Main Authors Wang, Weiji, Qian, Wei, Bai, Yuguang, Wang, Kunming
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.05.2023
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