Gas-kinetic BGK scheme for hypersonic flow simulation
In this paper, the BGK (Bhatnagar-Gross-Krook) scheme is extended to hypersonic flow simulations and thus shows that the compressible inviscid flow solutions of the simulations are efficiently and accurately obtained from the BGK scheme without the disastrous shock instability phenomenon that occurs...
| Published in: | Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting |
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| Main Author: | |
| Format: | Conference paper |
| Language: | English |
| Published: |
2006
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| Online Access: | https://www.scopus.com/inward/record.uri?eid=2-s2.0-34250767313&partnerID=40&md5=c626128f2b72142cac0619ab60d61ba8 |