Spherical Source Flow with a Finite Back Pressure.

Abstract

The interaction of a hypersonic spherical source flow with a rarefied background is investigated using the Boltzmann equation with model collision terms. Employing multi-fluid descriptions of the flow, it is found that two length scales are important in describing the interaction as the background becomes increasingly rarefied. Background scattering occurs on one scale and jet scattering on the other. Matched asymptotic expansions of the variables in the two regions are developed and first order composite solutions constructed. These solutions describe the transition away from the perfect vacuum limit of the expanding flow. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1972
Accession Number
AD0741989

Entities

People

  • B. B. Hamel
  • John W. Brook

Organizations

  • Grumman

Tags

DTIC Thesaurus Topics

  • Asymptotic Series
  • Back Pressure
  • Boltzmann Equation
  • Collisions
  • Composite Materials
  • Cooperation
  • Equations
  • Mathematics
  • Scattering
  • Transitions

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight