Dimotakis, Paul E. and Hall, Jeffery L. (1987) A Simple Model for Finite Chemical Kinetics Analysis of Supersonic Turbulent Shear Layer Combustion. In: AIAA/ASME/SAE/ASEE 23rd Joint Propulsion Conference. American Institute of Aeronautics and Astronautics , New York, NY. https://resolver.caltech.edu/CaltechAUTHORS:20141020-150416296
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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 Damköhler number effects in such flows. Sample calculations and comparisons for the H_2/NO/F_2 chemical system and the H_2/air system are described for a set of initial flow and thermodynamic conditions of the entrained reactants.
Item Type: | Book Section | |||||||||
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Additional Information: | Copyright (1987) by J. L. Hall and P. E. Dimotakis. AIAA-87-1879. We would like to acknowledge the helpful discussions with Dr. G. Mungal. The work was supported by AFOSR Grant No. 83-0213. | |||||||||
Group: | GALCIT | |||||||||
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DOI: | 10.2514/6.1987-1879 | |||||||||
Record Number: | CaltechAUTHORS:20141020-150416296 | |||||||||
Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20141020-150416296 | |||||||||
Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | |||||||||
ID Code: | 50570 | |||||||||
Collection: | CaltechAUTHORS | |||||||||
Deposited By: | INVALID USER | |||||||||
Deposited On: | 20 Oct 2014 22:19 | |||||||||
Last Modified: | 10 Nov 2021 18:57 |
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