Hypersonic flow simulation by the gas-kinetic bhatnagar-gross-krook scheme
The gas-kinetic Bhatnagar–Gross–Krook (BGK) 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 in...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
The American Institute of Aeronautics and Astronautics (AIAA)
2005
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/5934/ http://irep.iium.edu.my/5934/ http://irep.iium.edu.my/5934/4/waqar_1.11174.fp.pdf |