Abstract
The rotational nonequllibrium effect is taken into account by introducing excess normal stress associated with the bulk viscosity of the gas. The computational model for diatomic gases reduces to the model for monatomic gases in the limit of vanishing bulk viscosity. The thermodynamically consistent computational model is applied to the one-dimensional shock wave structure and the two-dimensional hypersonic rarefied flow around a blunt body in order to demonstrate its capability and validate the numerical results.
| Original language | English |
|---|---|
| Publication status | Published - 2006 |
| Event | 3rd International Conference for Mesoscopic Methods in Engineering and Science - Virginia, USA Duration: 25 Jul 2006 → 28 Jul 2006 |
Conference
| Conference | 3rd International Conference for Mesoscopic Methods in Engineering and Science |
|---|---|
| City | Virginia, USA |
| Period | 25/07/06 → 28/07/06 |
Keywords
- gas flow
- heat transfer
- hydrodynamics
- microchannels
Fingerprint
Dive into the research topics of 'Hydrodynamic descriptions of curious non-equilibrium phenomena in hypersonic and microscale gas flows'. Together they form a unique fingerprint.Projects
- 2 Finished
-
A High-Order Continuum Model for Computational Hypersonic Aerodynamics
Reese, J. (Principal Investigator)
EPSRC (Engineering and Physical Sciences Research Council)
1/09/04 → 30/09/07
Project: Research
-
Fluid Flow and Heat Transfer in Gas Microsystems
Reese, J. (Principal Investigator)
EPSRC (Engineering and Physical Sciences Research Council)
1/01/04 → 30/09/07
Project: Research
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