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