On the Mixing Problem of an Axi-Symmetric Free Jet into Air Including Chemical Reactions

Abstract

Velocity and temperature fields together with specie concentrations are computed for an axially symmetric, supersonic, hot, free jet mixing with quiescent air. Based on simplifying assumptions regarding the chemistry involved, the problem can be divided in two parts. One of these parts is to determine the velocity and temperature field. The second part consists of integrating the continuity of the specie equations when the solution to the first part of the problem is obtained. Two different cases are considered frozen and equilibrium flow.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1961
Accession Number
AD0257890

Entities

People

  • Inge L. Ryhming

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Pressure
  • Chemical Equilibrium
  • Chemical Reaction Properties
  • Chemical Reactions
  • Coefficients
  • Combustion
  • Combustion Chambers
  • Computational Science
  • Continuity
  • Diffusion Coefficient
  • Equations
  • Equations Of Motion
  • Flow Fields
  • Fluid Mechanics
  • Prandtl Number
  • Temperature Gradients
  • Turbulent Mixing

Readers

  • Calculus or Mathematical Analysis
  • Combustion and Flow Dynamics.
  • Organic Chemistry

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow