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本文介绍弯曲壁面上湍流边界层与正激波干涉的某些计算结果。壁面曲率对激波前后的压力比有重要影响。在干涉区中,边界层位移、动量和能量厚度都有显著的增加。这种增加主要决定于激波前后的压力比。(TBTF)
This paper introduces some results of the turbulent boundary layer on the curved wall and the interference of the forward shock wave. Wall curvature has an important effect on the pressure ratio before and after the shock wave. In the interference zone, the boundary layer displacement, momentum and energy thickness have significantly increased. This increase is mainly determined by the pressure ratio before and after the shock wave. (TBTF)