INCOMPRESSIBLE LAMINAR BOUNDARY LAYERS ON A PARABOLA AT ANGLE OF ATTACK: A STUDY OF THE SEPARATION POINT,

Abstract

The laminar boundary-layer equations were solved for incompressible flow past a parabola at angle of attack. Such flow experiences a region of adverse pressure gradient and thus can be employed to study the boundary-layer separation process. The present solutions were obtained numerically using both implicit and Crank Nicholson type difference schemes. It was found that in all cases the point of vanishing shear stress (the separation point) displayed a Goldstein type singularity. Based on this evidence, it is concluded that a singularity is always present at separation independent of the mildness of the pressure gradient at that point. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1970
Accession Number
AD0712084

Entities

People

  • M. J. Werle
  • R. T. Davis

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Equations
  • Flow
  • Incompressible Flow
  • Laminar Boundary Layer
  • Layers
  • Pressure Gradients
  • Shear Stresses
  • Stresses

Fields of Study

  • Physics

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Mechanics and Fluid Dynamics.