Calculation of the Laminar Boundary Layer on a Slipping Wing by the Method of Integral Relationships,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Pagination or Media Count:
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.
- Fluid Mechanics