RADIATION COUPLED WEDGE FLOW USING METHOD OF INTEGRAL RELATIONS,

Abstract

The radiation coupled supersonic flow past a wedge (or cone) is formulated using the first approximation of the method of integral relations. Solutions obtained for wedge flow of an optically thin, i.e. nonabsorbing, gas indicate a temperature decrease and density increase along the surface with a corresponding shock wave decay. Radiation effects on velocity and pressure are relatively small. Anamolous behavior of the transparent gas far downstream of the leading edge suggests a criterion for estimating the region of validity for the optically thin gas approximation. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1965
Accession Number
AD0624554

Entities

People

  • Martin C. Jischke

Organizations

  • Massachusetts Institute of Technology

Tags

DTIC Thesaurus Topics

  • Flow
  • Integrals
  • Leading Edges
  • Radiation
  • Radiation Effects
  • Shock
  • Shock Waves
  • Supersonic Flow
  • Waves

Fields of Study

  • Physics

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight