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A Simple Model for Finite Chemical Kinetics Analysis of Supersonic Turbulent Shear Layer Combustion

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. http://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
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.2514/6.1987-1879DOIArticle
http://arc.aiaa.org/doi/abs/10.2514/6.1987-1879PublisherArticle
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
Funders:
Funding AgencyGrant Number
Air Force Office of Scientific Research (AFOSR)83-0213
Record Number:CaltechAUTHORS:20141020-150416296
Persistent URL:http://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: Kristin Buxton
Deposited On:20 Oct 2014 22:19
Last Modified:21 Sep 2016 23:05

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