Accession Number : AD0763285
Title : Calculation of the Laminar Boundary Layer on a Slipping Wing by the Method of Integral Relationships,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Barinov,V. A.
Report Date : 18 JUN 1973
Pagination or Media Count : 13
Abstract : A numerical method is described for the calculation of equations for an incompressible three-dimensional boundary layer on a slipping wing. It is a development of the method of integral relationships of A. A. Dorodnitsyn. Examples are given for the calculation of two flows - with suction of a gas across a surface and without suction. The results obtained using this method practically coincide with the results of calculation by the finite-difference method.
Descriptors : (*LAMINAR BOUNDARY LAYER, NUMERICAL ANALYSIS), THREE DIMENSIONAL FLOW, INCOMPRESSIBLE FLOW, WINGS, PARTIAL DIFFERENTIAL EQUATIONS, DIFFERENCE EQUATIONS, USSR, EQUATIONS OF MOTION
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE