GAS DYNAMICS OF HIGH-ALTITUDE ROCKET PLUMES

Abstract

The report describes methods for calculation of the velocities and thermodynamic properties of flow fields through and around high altitude rocket plumes. The main effort is directed at obtaining a good representation of both the jet flow from rocket motors and the shock-mixing layers in the frontal regions; the calculation then proceeds downstream using standard methods. A comparison with available observations shows good agreement with overall plume dimensions as determined by the flow-field analysis. It may be concluded that the analysis provides a sound gas-dynamic description which may be used as a basis for investigation of the plasma and chemi-electric properties of high altitude plumes.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1964
Accession Number
AD0607940

Entities

People

  • Henry L. Alden
  • Roger H. Habert

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Asymptotic Series
  • Blunt Bodies
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Continuum Mechanics
  • Flow Fields
  • Fluid Dynamics
  • Geometry
  • Mechanics
  • Navier Stokes Equations
  • Physics Laboratories
  • Rocket Engines
  • Shock Waves
  • Stagnation Point
  • Thermodynamic Properties

Readers

  • Combustion and Flow Dynamics.
  • Plasma Physics / Magnetohydrodynamics
  • Regression Analysis.