Explicit expressions for the bulk force completely suppressing the crossflow in the three-dimensional boundary layer on a yawed wing in a uniform perfect-gas flow are derived. An optimum distribution of the suppressing force is found. The mixed problems of calculating the form of the distributed mechanical action and the parameters of the corresponding flow in the controlled boundary layer are formulated. The effect of the accompanying bulk heating on the suppression process is investigated.
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S. V. Manuĭlovich (2015) studied this question.
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