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改进 k-ω-γ 转捩模式对不同雷诺数下 HIAD 的转捩预测

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  • Release time:2023-02-24

  • Impact Factor:0.757

  • Journal:航空学报

  • Key Words:边界层转捩；转捩模式；柔性减速器；高超声速；气动热。

  • First Author:刘宏康

  • Indexed by:学术研究论文

  • Correspondence Author:zhaoyatian

  • Translation or Not:no

  • Date of Publication:2022-01-25

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