Aerodynamic interaction of heat transfer with steady transonic flow
Abstract
An experimental study investigated the interactive effect between the heat transfer and the steady transonic flow in a simple convergent-divergent duct. The results show that the position of the shock is considerably affected by the effect of wall cooling. The physical explanation for the shift is also offered. The results may have implications in the other internal flow problems.
- Publication:
-
AIAA, Aerospace Sciences Meeting
- Pub Date:
- January 1981
- Bibcode:
- 1981aiaa.meetU....K
- Keywords:
-
- Convergent-Divergent Nozzles;
- Ducted Flow;
- Heat Transfer;
- Steady Flow;
- Transonic Flow;
- Boundary Layer Flow;
- Flow Distribution;
- Inviscid Flow;
- Mach Number;
- Navier-Stokes Equation;
- Pressure Distribution;
- Shock Waves;
- Wall Temperature;
- Fluid Mechanics and Heat Transfer