IONIZATION IN AFTERBURNING ROCKET EXHAUSTS.

Abstract

A survey is presented relating existing knowledge of jet flow and mixing, including turbulence, in the continuum regime of fluid dynamics, to the afterburning rocket exhaust stream. Recent experimental information on ionization in flames is outlined, and consequences for ionization in rocket exhausts suggested. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1961
Accession Number
AD0603297

Entities

People

  • Felix T. Smith

Organizations

  • SRI International

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Afterburning
  • Computational Fluid Dynamics
  • Computational Science
  • Dynamics
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Fluids
  • Ionization
  • Jet Flow
  • Mechanics
  • Physics
  • Rocket Exhaust
  • Turbulence

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Plasma Physics.
  • Theoretical Analysis.