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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Published in | Thermal science and engineering progress Vol. 40; p. 101792 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.05.2023
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Subjects | |
Online Access | Get full text |
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