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...
Disimpan dalam:
| Pengarang-pengarang Utama: | , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Bahasa: | English |
| Diterbitkan: |
2006
|
| Subjek-subjek: | |
| Capaian Atas Talian: | http://eprints.utm.my/314/ http://eprints.utm.my/314/1/OngJChit2006_Gas-KineticBGKSchemeforSupersonicChannel.pdf |
| Penanda-penanda: |
Tambah Penanda
Tiada Penanda, Jadilah orang pertama menanda rekod ini!
|
Jadilah orang pertama meninggalkan komen!