Experimental study of heat transfer on flat plate during the interaction of oblique shock wave with laminar boundary layer
Abstract
Flat plates with two and three dimensional interactions of oblique shock waves with the boundary layer were studied. The correlation of the maximum values of heat flux in the range of the boundary layer connection was found.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- January 1975
- Bibcode:
- 1975STIN...7532412K
- Keywords:
-
- Flat Plates;
- Heat Transfer;
- Laminar Boundary Layer;
- Shock Waves;
- Aerodynamic Heating;
- Hypersonic Flow;
- Supersonic Flow;
- Fluid Mechanics and Heat Transfer