Accession Number : ADA195165
Title : Studies of Gas Turbine Heat Transfer Airfoil Surface and End-Wall Cooling Effects.
Descriptive Note : Annual rept. Mar 87-Mar 88,
Corporate Author : MINNESOTA UNIV MINNEAPOLIS DEPT OF MECHANICAL ENGINEERING
Personal Author(s) : Eckert, E R ; Goldstein, R J ; Patankar, S V ; Simon, T W
PDF Url : ADA195165
Report Date : Mar 1988
Pagination or Media Count : 58
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.
Descriptors : *AIRFOILS, *FILM COOLING, *HEAT TRANSFER, *TURBULENT BOUNDARY LAYER, ADIABATIC CONDITIONS, COOLING, CURVATURE, FLAT PLATE MODELS, HOLES(OPENINGS), MATHEMATICAL PREDICTION, MEASUREMENT, NUMERICAL METHODS AND PROCEDURES, RECOVERY, SURFACES, TURBULENCE, WALLS
Subject Categories : Thermodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE