A decomposition formula for the wall heat flux of a compressible boundary layer

Abstract Understanding the generation mechanism of the heat flux is essential for the design of hypersonic vehicles. We proposed a novel formula to decompose the heat flux coefficient into the contributions of different terms by integrating the conservative equation of the total energy. The reliabil...

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Autores principales: Dong Sun, Qilong Guo, Xianxu Yuan, Haoyuan Zhang, Chen Li, Pengxin Liu
Formato: article
Lenguaje:EN
Publicado: SpringerOpen 2021
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Acceso en línea:https://doaj.org/article/80f7f5b80b324dffb455befad500b18a
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