超音速
湍流
边界层
机械
物理
边界(拓扑)
曲面(拓扑)
边界层厚度
直接数值模拟
几何学
数学
数学分析
雷诺数
作者
Xiaoshuai Wu,Jianhan Liang,Yuxin Zhao
标识
DOI:10.1103/physrevfluids.4.044602
摘要
An investigation finds that a supersonic turbulent boundary layer is highly destabilized by a longitudinal concave surface. The intensification of vortical structures reflects the effect of turbulence amplification. Streaky turbulent motions suggest enhanced inner-outer interactions.
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