Abstract
During re-entry, a spacecraft will experience flow conditions ranging from highly rarefied to continuum. To simulate regions in between, a hydrodynamic-molecular gas hybrid solver should be used to provide accuracy and effciency. Currently available hybrid codes are in-house codes or do not provide the capabilities to simulate all of the phenomena a spacecraft will experience during re-entry. An open-source CFD-DSMC hybrid code is being developed within the OpenFOAM framework, coupling the solvers dsmcFoam and hy2Foam. In this paper, comparison between the CFD, DSMC and hybrid codes have been performed for simple cases. The dsmcFoam and the hybrid code have shown to compare satisfactorily.
Original language | English |
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Title of host publication | Proceedings of the 30th International Symposium on Rarefied Gas Dynamics |
Editors | Henning Struchtrup, Andrew Ketsdever |
Place of Publication | Melville, N.Y. |
Number of pages | 8 |
Volume | 1786 |
DOIs | |
Publication status | Published - 15 Nov 2016 |
Event | 30th International Symposium on Rarefied Gas Dynamics - University of Victoria, Victoria BC, Canada Duration: 10 Jul 2016 → 15 Jul 2016 https://conferences.uvic.ca/index.php/rgd/RGD30 |
Publication series
Name | AIP Conference Proceedings |
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Publisher | AIP |
Volume | 1786 |
Conference
Conference | 30th International Symposium on Rarefied Gas Dynamics |
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Country/Territory | Canada |
City | Victoria BC |
Period | 10/07/16 → 15/07/16 |
Internet address |
Keywords
- space vehicles
- flow simulations
- re-entry
- highly-rarefied regime
- continuum
- hybrid solvers
- spacecraft
- OpenFOAM
- computational fluid dynamics
- direct simulation Monte Carlo