Published 1987
| Published
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A Simple Model for Finite Chemical Kinetics Analysis of Supersonic Turbulent Shear Layer Combustion
- Creators
- Dimotakis, Paul E.
- Hall, Jeffery L.
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.
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.Attached Files
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Additional details
- Eprint ID
- 50570
- Resolver ID
- CaltechAUTHORS:20141020-150416296
- 83-0213
- Air Force Office of Scientific Research (AFOSR)
- Created
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2014-10-20Created from EPrint's datestamp field
- Updated
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2021-11-10Created from EPrint's last_modified field
- Caltech groups
- GALCIT