Studies of Gas Turbine Heat Transfer Airfoil Surface and End-Wall Cooling Effects.
Abstract
Research results on curved surface heat transfer, airfoil heat transfer, film cooling and end-wall heat transfer are presented. In particular these studies focus on the recovery process of a turbulent boundary layer from curvature, heat transfer measurements and numerical prediction techniques of film-cooling on an adiabatic flat plate by injection through a single row of holes. Keywords: Heat transfer, Turbulence.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1988
- Accession Number
- ADA195165
Entities
People
- E. R. Eckert
- R. J. Goldstein
- S. V. Patankar
- Terrence W. Simon
Organizations
- University of Minnesota