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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Dettagli Bibliografici
Autori principali: Dong Sun, Qilong Guo, Xianxu Yuan, Haoyuan Zhang, Chen Li, Pengxin Liu
Natura: Articolo
Lingua:English
Pubblicazione: SpringerOpen 2021-11-01
Serie:Advances in Aerodynamics
Soggetti:
Accesso online:https://doi.org/10.1186/s42774-021-00081-y