STRONG INTERACTION WITH SLIP BOUNDARY CONDITIONS

Abstract

A solution to the problem of strong interaction between the shock wave and the boundary layer has been obtained for the case where velocity slip and temperature jump boundary conditions are consistent at the wall. It is shown that the addition of slip boundary conditions yields a correction of order (boundary layer thickness/X) to the no slip solution. Estimates are made of the effect of slip on induced pressures and skin friction for the case of the adiabatic wall. In addition, it is shown that the inclusion of slip boundary conditions does not change the energy transfer to the wall from the no slip values. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1961
Accession Number
AD0269539

Entities

People

  • J. Aroesty

Organizations

  • University of California, Berkeley

Tags

Communities of Interest

  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Boundary Layer
  • Coefficients
  • Differential Equations
  • Displacement
  • Energy
  • Energy Transfer
  • Flow Fields
  • Fluid Dynamics
  • Friction
  • Heat Transfer
  • Mean Free Path
  • Pressure Gradients
  • Shear Stresses
  • Shock Waves
  • Skin Friction

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Plasma Physics / Magnetohydrodynamics