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