Accession Number:

AD0763285

Title:

Calculation of the Laminar Boundary Layer on a Slipping Wing by the Method of Integral Relationships,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Barinov,V. A.

Report Date:

1973-06-18

Pagination or Media Count:

13.0

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