FoamDSMC: An object oriented parallel DSMC solver for rarefied flow applications

Jeffrey Allen, Thomas Hauser

    Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

    8 Scopus citations

    Abstract

    The prevalence of applications involving the simulation of rarefied gas flows continues to increase. As such, new and innovative means for their solution have become necessary. Presented herein, is a new, parallel, steady/unsteady direct simulation Monte Carlo solver, foamDSMC, based on object oriented programming practice. Its development, and validation are presented, along with various single and multiple processor performance characteristics. The validation results, of both the hypersonic corner flow and sphere flow, showed the accuracy of the solver to be comparable to commercial solvers. The foamDSMC solver was additionally applied to a sounding rocket flight, and thus showed its applicability to practical simulations. The single and multiple processor performance results demonstrated good scalability with increased problem sizes and clear avenues for future improvements.

    Original languageEnglish
    Title of host publicationCollection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
    Pages13351-13365
    Number of pages15
    StatePublished - 2007
    Event45th AIAA Aerospace Sciences Meeting 2007 - Reno, NV, United States
    Duration: Jan 8 2007Jan 11 2007

    Publication series

    NameCollection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
    Volume19

    Conference

    Conference45th AIAA Aerospace Sciences Meeting 2007
    Country/TerritoryUnited States
    CityReno, NV
    Period01/8/0701/11/07

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