Film cooling heat transfer on a turbine airfoil
Abstract
The objectives of the current program are to develop an analytical approach, based on boundary layer theory, for predicting the effects of airfoil cooling on downstream heat transfer rates and to verify the resulting analytical method by comparison of predictions with hot cascade data obtained under this program.
- Publication:
-
Turbine Engine Hot Section Technology, 1985
- Pub Date:
- October 1985
- Bibcode:
- 1985tehs.nasa..151H
- Keywords:
-
- Airfoils;
- Boundary Layers;
- Film Cooling;
- Heat Transfer;
- Turbine Engines;
- Cascade Flow;
- Mathematical Models;
- Proving;
- Rates (Per Time);
- Fluid Mechanics and Heat Transfer