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...
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| தலைமை எழà¯à®¤à¯à®¤à®¾à®³à®°à¯à®•ளà¯: | , , , |
|---|---|
| வடிவமà¯: | Conference or Workshop Item |
| மொழி: | English |
| வெளியீடபà¯à®ªà®Ÿà¯à®Ÿà®¤à¯: |
2006
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| பகà¯à®¤à®¿à®•ளà¯: | |
| நிகழà¯à®¨à®¿à®²à¯ˆ அணà¯à®•லà¯: | http://eprints.utm.my/314/ http://eprints.utm.my/314/1/OngJChit2006_Gas-KineticBGKSchemeforSupersonicChannel.pdf |
| கà¯à®±à®¿à®¯à¯€à®Ÿà¯à®•ளà¯: |
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