Introduction
This paper describes the application of a new DSMC code, called dsmcFoam, which has been written within the framework of the open-source computational fluid dynamics (CFD) toolbox OpenFOAM[1]. The main features of dsmcFoam are its C++ modularity, its unlimited parallel processing capability and its ability to easily handle arbitrary, complex 3D geometries. Results of initial benchmark trials [2] have shown excellent agreement with both analytical solutions and other conventional DSMC codes.
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References
OpenFOAM: The open source CFD toolbox, user guide, version 1.6 (2009), http://www.openfoam.com
Scanlon, T.J., Roohi, E., White, C., Darbandi, M., Reese, J.M.: An open source, parallel DSMC code for rarefied gas flows in arbitrary geometries. Computers and Fluids 39(10), 2078–2089 (2010)
Bird, G.A.: Molecular Gas Dynamics and the Direct Simulation of Gas Flows. Clarendon, Oxford (2009)
Bird, G.A.: Definition of mean free path in real gases. Physics of Fluids 26(11), 3222–3223 (1983)
Holden, M.S., Wadhams, T.P., Candler, G.V., Harvey, J.K.: Measurements in regions of low density laminar shock wave/ boundary layer interaction in hypervelocity flows and comparison with Navier-Stokes predictions. AIAA Paper 2003-1131 (2003)
Moss, J.N., Bird, G.A., Markelov, G.N.: DSMC simulations of hypersonic flows and comparison with experiments. In: AIP Conference Proceedings, vol. 762, pp. 547–552 (2004)
Allègre, J., Bisch, D., Lengrand, J.C.: Experimental rarefied density flowfields at hypersonic conditions over 70-degree blunted cone. Journal of Spacecraft and Rockets 34(6), 714–718 (1997)
Allègre, J., Bisch, D., Lengrand, J.C.: Experimental rarefied aerodynamic forces at hypersonic conditions over 70-degree blunted cone. Journal of Spacecraft and Rockets 34(6), 719–723 (1997)
Allègre, J., Bisch, D., Lengrand, J.C.: Experimental rarefied heat transfer at hypersonic conditions over 70-degree blunted cone. Journal of Spacecraft and Rockets 34(6), 724–728 (1997)
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Ahmad, A.O., Scanlon, T.J., Reese, J.M. (2012). Benchmarking a New, Open-Source Direct Simulation Monte Carlo (DSMC) Code for Hypersonic Flows. In: Kontis, K. (eds) 28th International Symposium on Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-25685-1_164
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DOI: https://doi.org/10.1007/978-3-642-25685-1_164
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