Studies of Gas Turbine Heat Transfer Airfoil Surface and End-Wall.
Annual progress rept. 28 Feb 86-1 Apr 87,
MINNESOTA UNIV MINNEAPOLIS DEPT OF MECHANICAL ENGINEERING
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This report documents work on the topic of heat transfer from gas turbine airfoil, end-wall and internal passage surfaces. The research is divided into the following subtopics curvature effects, including transition and film cooling and airfoil heat transfer, including portions near the endwall. Keywords Cascade structures End-all curvature.
- Jet and Gas Turbine Engines
- Fluid Mechanics