DIFFUSION FLAMES AND SUPERSONIC COMBUSTION.

Abstract

The method of matched asymptotic expansions has been used for the analysis of the H2-Air reaction in the temperature and pressure range of interest to Supersonic Combustion. The use of the method is advantageous because of the large differences in the rate constants of the elementary reactions appearing in the reaction mechanism. The ratios between the rate constants are used as the small or large parameter in the perturbation method. Several stages are found in the course of the reaction and at each stage only a small number of the elementary reactions play an important role. Different expansions are used for each stage, and they are matched according to the rules of the method of matched asymptotic expansion of Kaplun, Lagerstron, etc. For the zeroth order approximation, at each stage, the reaction mechanism is very often drastically simplified. This occurs because some of the elementary reactions are 'frozen' while others are at equilibrium; some species are not changing at a given stage, while others take a quasi-steady state value. Very often an overall reaction rate may be used for the zeroth order approximation at each stage. The method of matched asymptotic expansions allows to determine how the appropriate overall reaction rate changes with the succesive stages of the reaction and with the initial stoichiometry of the mixture. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1969
Accession Number
AD0693341

Entities

People

  • A. Linan
  • E. Fraga
  • I. Da-riva
  • J. Urrutia

Tags

DTIC Thesaurus Topics

  • Asymptotic Series
  • Burning Rate
  • Chemical Reaction Properties
  • Chemical Reactions
  • Combustion
  • Diffusion
  • Endothermic Reactions
  • Exothermic Reactions
  • Perturbations
  • Reaction Mechanisms
  • Steady State
  • Stoichiometry
  • Supersonic Combustion

Fields of Study

  • Mathematics

Readers

  • Applied Combinatorial Optimization and Logic Circuit Design.
  • Calculus or Mathematical Analysis
  • Combustion science or combustion engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight