Numerical study on the influence of wall temperature gradient on aerodynamic characteristics of low aspect ratio flying wing configuration

Abstract With the aim for a low-aspect-ratio flying wing configuration, this study explores the influence of wall temperature gradient on the laminar and turbulent boundary layers of aircraft surface and determines the effect on the transition Reynolds number and wall friction drag. A four-equation...

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Autores principales: Peng Lin, Xueqiang Liu, Neng Xiong, Xiaobing Wang, Ma Shang, Guangyuan Liu, Yang Tao
Formato: article
Lenguaje:EN
Publicado: Nature Portfolio 2021
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Acceso en línea:https://doaj.org/article/66e4016d41dc47bfada51f979e77cf39
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