Gas Kinetic Scheme Coupled with High-Speed Modifications for Hypersonic Transition Flow Simulations

The issue of hypersonic boundary layer transition prediction is a critical aerodynamic concern that must be addressed during the aerodynamic design process of high-speed vehicles. In this context, we propose an advanced mesoscopic method that couples the gas kinetic scheme (GKS) with the Langtry–Men...

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Hlavní autoři:	Chengrui Li, Wenwen Zhao, Hualin Liu, Youtao Xue, Yuxin Yang, Weifang Chen
Médium:	Artigo
Jazyk:	Inglês
Vydáno:	MDPI AG 2024-02-01
Edice:	Entropy
Témata:	boundary layers transition flow gas kinetic scheme hypersonic flow turbulence models
On-line přístup:	https://www.mdpi.com/1099-4300/26/2/173
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