Accession Number : AD0763280

Title :   Three Dimensional Boundary Layer in the Vicinity of a Critical Line of a Slipping Wing during Nonuniform Suction,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Barinov,V. A.

Report Date : 20 JUN 1973

Pagination or Media Count : 15

Abstract : 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.

Descriptors :   (*SWEPT WINGS, *TURBULENCE), (*BOUNDARY LAYER CONTROL, SUCTION SLOTS), NUMERICAL METHODS AND PROCEDURES, EQUATIONS OF MOTION, THREE DIMENSIONAL FLOW, STATISTICAL DISTRIBUTIONS, USSR

Subject Categories : Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE