Three Dimensional Boundary Layer in the Vicinity of a Critical Line of a Slipping Wing during Nonuniform Suction,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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A numerical method is described for calculating the equations of an incompressible boundary layer, which is a generalization of the method of integral relations of A. A. Dorodnitsyn for a three-dimensional boundary layer. Presented are the results for calculating the characteristics of the boundary layer for the various distribution laws of suction intensity on the leading edge along the wing span.