High fidelity modeling of energy transfer and chemical reactions in shock waves

Tong Zhu, Zheng Li, Neal Parsons, Deborah A. Levin

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

Abstract

In this work, newly-developed MD-QCT databases1 for chemical reaction and interal energy relaxation are implemented progressively in DSMC simulations of heat bath cases and normal shocks in nitrogen and the results are compared with those obtained using the traditional TCE and LB models. In the heat bath cases the MD-QCT chemical reaction model predicts more dissociation and less nonequilibrium eventually and faster relaxation of the vibrational temperature compared with using the TCE-LB models. In the lower speed one-dimensional unsteady shocks cases, the flow field results exhibit similar behavior as those seen in the heat bath case when the MD-QCT databases are progressively added. Finally, in the even higher speed shock conditions as those appeared in the experiments by Fujita et al., the use of MD-QCT databases for both chemical reaction and interal energy predicts more dissociation in the downstream of the shock but slower relaxation of the rotational temperature than using the TCE and LB models. Furthermore, the rotational temperature in the shock region is in better agreement with experiments and confirms that large rotational nonequilibrium is present in very strong nitrogen shocks.

Original languageEnglish (US)
Title of host publicationAIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624102936
DOIs
StatePublished - 2014
Externally publishedYes
EventAIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference 2014 - Atlanta, GA, United States
Duration: Jun 16 2014Jun 20 2014

Publication series

NameAIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference

Other

OtherAIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference 2014
Country/TerritoryUnited States
CityAtlanta, GA
Period6/16/146/20/14

ASJC Scopus subject areas

  • Aerospace Engineering
  • Mechanical Engineering

Fingerprint

Dive into the research topics of 'High fidelity modeling of energy transfer and chemical reactions in shock waves'. Together they form a unique fingerprint.

Cite this