Simulation and Modeling of Hypersonic Turbulent Boundary Layers Subject to Adverse Pressure Gradients due to Streamline Curvature
Simulation and Modeling of Hypersonic Turbulent Boundary Layers Subject to Adverse Pressure Gradients due to Streamline Curvature
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DOI：
10.2514/6.2021-2891
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发表时间：
2021-07
期刊：
影响因子：
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通讯作者：
G. Nicholson;Junji Huang;L. Duan;Meelan Choudhari;R. Bowersox
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文献类型：
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作者：
G. Nicholson;Junji Huang;L. Duan;Meelan Choudhari;R. Bowersox
Ø边界层生长与实验报告的值非常吻合Ø与克劳瑟β参数的比较也很好
Ø Boundary layer growth closely matches values reported from experiments Ø Similarly good comparison is found with Clauser beta parameter