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Aerothermodynamic Optimization of Aerospace Plane Airfoil Leading Edge
Aiming to mitigate the aerodynamic heating during hypersonic re-entry, the aerothermodynamic optimization of aerospace plane airfoil leading edge is conducted. Lift-todrag ratio at landing condition is taken as a constraint to ensure the landing aerodynamic performance. First, airfoil profile is par...
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| 出版年: | Journal of Aerospace Technology and Management |
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| 主要な著者: | , , , |
| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
Ministério da Defesa
2017
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| 主題: | |
| オンライン･アクセス: | https://www.redalyc.org/articulo.oa?id=309457439011 https://www.redalyc.org/journal/3094/309457439011/ https://www.redalyc.org/journal/3094/309457439011/html/ https://www.redalyc.org/journal/3094/309457439011/309457439011.epub https://www.redalyc.org/journal/3094/309457439011/movil |
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