A simple model for finite chemical kinetics analysis of supersonic turbulent shear layer combustion
Abstract
A simple flow/thermodynamic model is proposed to describe finite chemical kinetic rate combustion in a turbulent supersonic shear layer for the purposes of assessing Damkoehler number effects in such flows. Sample calculations and comparisons for the H2/NO/F2 chemical system and the H2/air system are described for a set of initial flow and thermodynamic conditions of the entrained reactants.
 Publication:

23rd Joint Propulsion Conference
 Pub Date:
 June 1987
 Bibcode:
 1987jpsd.confQ....D
 Keywords:

 Reaction Kinetics;
 Shear Layers;
 Supersonic Combustion;
 Turbulent Mixing;
 Damkohler Number;
 Hydrogen Fuels;
 Hypersonic Combustion;
 Fluid Mechanics and Heat Transfer