VISCOUS HYPERSONIC FLOW WITH PARABOLIC AXIALLY SYMMETRIC SHOCK.

Abstract

The inverse problem of determining the flow field for parabolic axially symmetric shock with regard to interaction of the boundary layer with non-viscous flow is considered. For description of non-viscous flow, the theory of small displacements is used. On the basis of an analysis of the order of the quantities, the question is considered of the joining of the parameters of the boundary layer with the parameters of non-viscous flow. A statement of the problem is given permitting the consideration both of the interaction connected with the displacing influence of the boundary layer, and vortical interaction. Results are cited of numerical calculations of the flow fields between the solids and the shock wave. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1965
Accession Number
AD0629044

Entities

People

  • V. S. Nikolaev

Organizations

  • Georgia Tech

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Flow
  • Flow Fields
  • Hypersonic Flow
  • Inverse Problems
  • Layers
  • Shock
  • Shock Waves
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Plasma Physics / Magnetohydrodynamics
  • Theoretical Analysis.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers