## Abstract The heat transfer characteristics of supersonic to hypersonic gas flow in microchannels are numerically studied by solving a twoβdimensional NavierβStokes (NS) system of equations utilizing Maxwell's velocity slip with thermal creep, and a corresponding temperature jump relationship der
Simulation of supersonic and hypersonic flows
β Scribed by J. F. Milthorpe
- Publisher
- John Wiley and Sons
- Year
- 1992
- Tongue
- English
- Weight
- 832 KB
- Volume
- 14
- Category
- Article
- ISSN
- 0271-2091
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β¦ Synopsis
A simple convection algorithm for simulation of time-dependent supersonic and hypersonic flows of a perfect but viscous gas is described. The algorithm is based on conservation and convection of mass, momentum and energy in a grid of rectangular cells. Examples are given for starting flow in a shock tube and oblique shocks generated by a wedge at Mach numbers up to 30.4. Good comparisons are achieved with well-known perfect gas flows.
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