Abstract
Numerical treatments for addressing the scales associated with the chemical aspects of high-speed reacting flows are evaluated in a shock-induced combustion flow field. The error associated with the source term is found to be correlated to the cell Damkohler number. Both a scaling and an interpolation method are evaluated and are found to improve the comparison between a computed flow field and experimental data. Performance of the methods are also found to be dependent on the particular reaction scheme used in the modeling.
| Original language | English |
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| DOIs | |
| Publication status | Published - 1998 |
| Externally published | Yes |
| Event | 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 - Reno, United States Duration: 12 Jan 1998 → 15 Jan 1998 |
Conference
| Conference | 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 |
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| Country/Territory | United States |
| City | Reno |
| Period | 12/01/98 → 15/01/98 |
Bibliographical note
Publisher Copyright:© 1998 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.