Gas-Kinetic BGK Scheme for Supersonic Channel Flow Simulation
In this paper, the gas-kinetic BGK (Bhatnagar-Gross-Krook) scheme is developed for simulating compressible inviscid supersonic channel flow. BGK scheme is an approximate Riemann solver that uses the collisional Boltzmann equation as the governing equation for flow evolutions. For efficient computati...
Saved in:
| Main Authors: | , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | en |
| Published: |
2006
|
| Subjects: | |
| Online Access: | http://eprints.utm.my/314/1/OngJChit2006_Gas-KineticBGKSchemeforSupersonicChannel.pdf http://eprints.utm.my/314/ |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|