An integral method associated with direct and inverse mode is presented for the calculation of compressible turbulent boundarylayer 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。
2
In this article, bl model is used to study three typical cases of compressible turbulent boundarylayer, 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。
3
Inverse integral method is used for compressible turbulent boundarylayer.