The paper deals with the problem of constructing the distribution law of the normal component of injection velocity in a turbulent boundary layer at supersonic flow velocities. The problem is solved using the Dorodnitsyn generalized method of integral relations and the Lagrange formalism. The computational experiments conducted have shown the efficiency of optimal controls in comparison with the uniform law of injection.

中文翻译：

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超音速气流中可渗透圆柱面上湍流边界层的最优控制

本文研究了在超声速下在湍流边界层中建立射流速度正态分量分布规律的问题。使用Dorodnitsyn广义积分关系方法和Lagrange形式主义可以解决该问题。进行的计算实验表明，与均匀注射定律相比，最佳控制的效率。