Studies of Gas Turbine Heat Transfer: Airfoil Surface and End-Wall.
Abstract
The annual report documents progress at the University of Minnesota Heat Transfer Laboratory on the topic of heat transfer from gas turbine airfoil and end-wall surface. Subtopics are: Curvature effects, End-wall heat transfer and Near-end-wall heat transfer. Curvature effects on turbulent transport are shown for a smooth convex wall and for single-row film-cooled convex and concave walls. End-wall mass (heat) transfer coefficient contours show the horseshoe vortex, the passage vortex and an inner vortex.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1986
- Accession Number
- ADA172470
Entities
People
- E. R. Eckert
- R. J. Goldstein
- Terrence W. Simon
Organizations
- University of Minnesota