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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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| Udgivet i: | AIAA J |
|---|---|
| Main Authors: | , , |
| Format: | Artigo |
| Sprog: | Inglês |
| Udgivet: |
2018
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| Fag: | |
| Online adgang: | 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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