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Direct Numerical Simulation Database for Hypersonic Turbulent Boundary Layers

In this paper, we present a direct numerical simulation database of high-speed zero-pressure-gradient turbulent boundary layers developing spatially over a flat plate with nominal freestream Mach number ranging from 2.5 to 14 and wall-to-recovery temperature ranging from 0.18 to 1.0. The flow condit...

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Detalhes bibliográficos
Publicado no:AIAA J
Main Authors: Zhang, Chao, Duan, Lian, Choudhari, Meelan M.
Formato: Artigo
Idioma:Inglês
Publicado em: 2018
Assuntos:
Acesso em linha:https://ncbi.nlm.nih.gov/pmc/articles/PMC7802740/
https://ncbi.nlm.nih.gov/pubmed/33442066
https://ncbi.nlm.nih.govhttp://dx.doi.org/10.2514/1.J057296
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