Study on the Leading Edge of a Hypersonic Vehicle Using the Aero-Thermoelastic Coupling Method
The characteristics of aero-thermoelastic coupling are important for the design of the leading edge in hypersonic vehicles. Herein, a fluid–structure interaction analysis is performed to study the leading edge of a hypersonic vehicle using aero-thermoelastic coupling methods. The results show that t...
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| Principais autores: | , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
MDPI AG
2022-12-01
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| coleção: | Aerospace |
| Assuntos: | |
| Acesso em linha: | https://www.mdpi.com/2226-4310/9/12/835 |
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