The endwall influence on heat transfer from a single cylinder - The horseshoe vortex effect
Abstract
An investigation is conducted on the influence of a horseshoe vortex on the stagnation region heat transfer characteristics of a two-dimensional bluff body (such as a gas turbine airfoil). A clse simulation of the various configurations of this phenomenon in engineering problems is found in a cylinder that intersects a plane plate in wind tunnel flow. Experimental results indicate increased heat transfer coefficient on the cylinder with increasing endwall upstream protrusion. For circumferential average heat transfer, a reversal of the effect of the endwall protrusion is noted; moreover, interactions of the horseshoe vortex flow with the flow in the separated region at the rear of the cylinder are found to make rational deductions and analyses difficult.
- Publication:
-
1983 Tokyo International Gas Turbine Congress
- Pub Date:
- 1984
- Bibcode:
- 1984gatu....1...23H
- Keywords:
-
- Circular Cylinders;
- Flow Distribution;
- Heat Transfer Coefficients;
- Rectangular Plates;
- Vortices;
- Wall Flow;
- Leading Edges;
- Low Speed Wind Tunnels;
- Reynolds Number;
- Stagnation Point;
- Temperature Measurement;
- Turbine Blades;
- Fluid Mechanics and Heat Transfer