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Physics-guided airfoil optimization design for shock buffet suppression

Abstract Shock buffet is one of the common flow instability problems in aviation engineering, which can affect flight handling quality and limit flight envelope. In this study, we propose a physics-guided aerodynamic optimization design framework to improve the buffet onset in the transonic region....

Täydet tiedot

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Bibliografiset tiedot
Päätekijät: Qiyue Ma, Chuanqiang Gao, Xiaojing Wu, Weiwei Zhang
Aineistotyyppi: Artigo
Kieli:Inglês
Julkaistu: SpringerOpen 2026-02-01
Sarja:Advances in Aerodynamics
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Linkit:https://doi.org/10.1186/s42774-025-00228-1
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