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

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 turbulenc...

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Detalles Bibliográficos
Autores principales: Lin, Peng, Liu, Xueqiang, Xiong, Neng, Wang, Xiaobing, Shang, Ma, Liu, Guangyuan, Tao, Yang
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Nature Publishing Group UK 2021
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8357923/
https://www.ncbi.nlm.nih.gov/pubmed/34381068
http://dx.doi.org/10.1038/s41598-021-94261-x

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8357923/
https://www.ncbi.nlm.nih.gov/pubmed/34381068
http://dx.doi.org/10.1038/s41598-021-94261-x

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