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

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.

Document Details

Document Type
Technical Report
Publication Date
Jun 20, 1973
Accession Number
AD0763280

Entities

People

  • V. A. Barinov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Equations
  • Integrals
  • Intensity
  • Layers
  • Leading Edges
  • Mathematics
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.