D. F. Abzalilov, R. A. Valitov, and N. B. Il’inskii
Problems were posed and solved concerning the aerodynamic computation of the flow past an airfoil with an active boundary layer control device used to prevent flow separation. A moving wall, suction, or tangential blowing in the boundary layer was used as a flow control device. The turbulent...
ISSN 09655425, Computational Mathematics and Mathematical Physics, 2009, Vol. 49, No. 12, pp....