An integral method associated with direct and inverse mode is presented for the calculation of compressible turbulent boundary layer with separations over airfoil.
本文介绍了一种求解二维可压缩紊流分离边界层的正反积分方法。
In this article, bl model is used to study three typical cases of compressible turbulent boundary layer, for which, data from direct numerical simulation (DNS) are available for comparison.
本文以BL模型为例，通过可压缩湍流边界层的三个典型算例，与直接数值模拟(DNS)的结果作对比。
Inverse integral method is used for compressible turbulent boundary layer.
湍流边界层采用积分反方法。
Inverse integral method is used for compressible turbulent boundary layer.
湍流边界层采用积分反方法。
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