EXACT SOLUTIONS FOR NONEQUILIBRIUM EXPANSIONS OF AIR WITH COUPLED CHEMICAL REACTIONS

Abstract

Results of numerical integrations of the coupled chemical rate equations and gasdynamic equations are presented for nozzle airflows. Composition histories are shown for a kinetic mechanism including 6 species and 14 reactions. The freezing process is complex because the N-O shuffle reactions couple the disociation-recombination reactions. In many cases where the energy in N dissociation is significant, the fast shuffle reactions prevent N atom freezing which would otherwise occur if 3 body recombination were the only process operating. Nitric oxide concentrations undershoot the equilibrium values in many cases. Oxygen freezing is affected little by the shuffle reactions. Results suggest the applicability of simplified chemical kinetic models based on the shuffle reactions for airflows in various regimes of the initial state.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1961
Accession Number
AD0257396

Entities

People

  • Alan Q. Eschenroeder
  • Donald W. Boyer
  • J. G. Hall

Organizations

  • Calspan

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Force
  • Chemical Composition
  • Chemical Reaction Properties
  • Chemical Reactions
  • Chemistry
  • Contracts
  • Dissociation
  • Efficiency
  • Enthalpy
  • Fluid Mechanics
  • Gases
  • Hypersonic Nozzles
  • Mach Number
  • Mechanics
  • Reynolds Number
  • Shock Tunnels

Readers

  • Combustion science or combustion engineering.
  • Control Systems Engineering.