Implementation of a chemical kinetics model for hypersonic flows in air for high-performance cfd

Research output: Chapter in Book/Report/Conference proceedingConference contribution

54 Scopus citations

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 languageEnglish (US)
Title of host publicationAIAA Scitech 2020 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105951
DOIs
StatePublished - 2020
EventAIAA Scitech Forum, 2020 - Orlando, United States
Duration: Jan 6 2020Jan 10 2020

Publication series

NameAIAA Scitech 2020 Forum
Volume1 PartF

Conference

ConferenceAIAA Scitech Forum, 2020
Country/TerritoryUnited States
CityOrlando
Period1/6/201/10/20

Bibliographical note

Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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