Abstract
The Modified Marrone-Treanor (MMT) chemical kinetics model [1] was developed recently using ab-initio quantum chemistry data. The MMT model has been implemented into a CFD code designed for hypersonic flows, with an emphasis on vehicle-scale calculation. The current feature set includes implicit time-stepping, recombination, electronic energy, and performance comparable to the standard Park model. The effect of non-Boltzmann distributions on chemical kinetics source terms are also quantified, and a relatively simple factor is found to be suitable for correcting the reaction rate and vibrational energy change per dissociation. Larger-scale CFD results are also presented and compared to the standard Park model [2]; the peak heat flux on a Crew Exploration Vehicle (CEV) type geometry is found to be 10% higher for Park than MMT.
| Original language | English (US) |
|---|---|
| Title of host publication | AIAA Scitech 2020 Forum |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624105951 |
| DOIs | |
| State | Published - 2020 |
| Event | AIAA Scitech Forum, 2020 - Orlando, United States Duration: Jan 6 2020 → Jan 10 2020 |
Publication series
| Name | AIAA Scitech 2020 Forum |
|---|---|
| Volume | 1 PartF |
Conference
| Conference | AIAA Scitech Forum, 2020 |
|---|---|
| Country/Territory | United States |
| City | Orlando |
| Period | 1/6/20 → 1/10/20 |
Bibliographical note
Publisher Copyright:© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
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