Heat transfer with very high free stream turbulence
Abstract
Stanton numbers as much as 350 percent above the accepted correlations for flat plate turbulent boundary layer heat transfer have been found in experiments on a low velocity air flow with very high turbulence (up to 50 percent). These effects are far larger that have been previously reported and the data do not correlate as well in boundary layer coordinates (Stanton number and Reynolds number) as they do in simpler coordinates: h vs. X. The very high relative turbulence levels were achieved by placing the test plate in different positions in the margin of a large diameter free jet. The large increases may be due to organized structures of large scale which are present in the marginal flowfield around a free jet.
- Publication:
-
Turbine Engine Hot Section Technology, 1985
- Pub Date:
- October 1985
- Bibcode:
- 1985tehs.nasa..203M
- Keywords:
-
- Cooling;
- Flat Plates;
- Flow Distribution;
- Free Jets;
- Gas Turbine Engines;
- Heat Transfer Coefficients;
- Turbulent Boundary Layer;
- Correlation;
- Reynolds Number;
- Stanton Number;
- Fluid Mechanics and Heat Transfer