Direct numerical simulation of high–temperature supersonic turbulent channel flow of equilibrium air
Direct numerical simulations (DNS) of high–temperature supersonic turbulent channel flow of equilibrium air are conducted at constant dimensional wall temperature 1733.2 K. The Mach number based on the bulk velocity and the speed of sound at the isothermal wall is 3.0, and the Reynolds number based...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
AIP Publishing LLC
2018-11-01
|
| Series: | AIP Advances |
| Online Access: | http://dx.doi.org/10.1063/1.5050657 |