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Abstract
An open source implementation of chemistry modelling for the direct simulation
Monte Carlo (DSMC) method is presented. Following the recent work of Bird [1] an approach known as the quantum kinetic (Q-K) method has been adopted to describe chemical reactions in a 5-species air model using DSMC procedures based on microscopic gas information. The Q-K technique has been implemented within the framework of the dsmcFoam code, a derivative of the open source CFD code OpenFOAM. Results for vibrational relaxation, dissociation and exchange reaction rates for an adiabatic bath demonstrate the success of the Q-K model when compared with analytical solutions for both inert and reacting conditions. A comparison is also made between the Q-K and total collision energy (TCE) chemistry approaches for a hypersonic flow benchmark case.
Monte Carlo (DSMC) method is presented. Following the recent work of Bird [1] an approach known as the quantum kinetic (Q-K) method has been adopted to describe chemical reactions in a 5-species air model using DSMC procedures based on microscopic gas information. The Q-K technique has been implemented within the framework of the dsmcFoam code, a derivative of the open source CFD code OpenFOAM. Results for vibrational relaxation, dissociation and exchange reaction rates for an adiabatic bath demonstrate the success of the Q-K model when compared with analytical solutions for both inert and reacting conditions. A comparison is also made between the Q-K and total collision energy (TCE) chemistry approaches for a hypersonic flow benchmark case.
Original language | English |
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Pages (from-to) | 1670-1680 |
Number of pages | 11 |
Journal | AIAA Journal |
Volume | 53 |
Issue number | 6 |
Early online date | 9 Apr 2015 |
DOIs | |
Publication status | Published - 30 Jun 2015 |
Keywords
- DSMC
- open source
- Chemistry
- non-equilibrium flow
- rarefied gas
- hypersonic flow
- OpenFOAM
Fingerprint
Dive into the research topics of 'Open source Direct Simulation Monte Carlo (DSMC) chemistry modelling for hypersonic flows'. Together they form a unique fingerprint.Projects
- 2 Finished
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International Collaboration Sabbatical - Beyond Navier-Stokes: computational gas dynamics for rarefied flow technologies
Scanlon, T. (Principal Investigator)
EPSRC (Engineering and Physical Sciences Research Council)
16/01/12 → 15/01/13
Project: Research
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Non-Equilibrium Fluid Dynamics for Micro/Nano Engineering Systems
Reese, J. (Principal Investigator)
EPSRC (Engineering and Physical Sciences Research Council)
1/01/11 → 16/02/16
Project: Research