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