Accession Number : ADA181558
Title : Studies of Gas Turbine Heat Transfer Airfoil Surface and End-Wall.
Descriptive Note : Annual progress rept. 28 Feb 86-1 Apr 87,
Corporate Author : MINNESOTA UNIV MINNEAPOLIS DEPT OF MECHANICAL ENGINEERING
Personal Author(s) : Eckert,Ernst R ; Goldstein,Richard J ; Simon,Terrence W
PDF Url : ADA181558
Report Date : Apr 1987
Pagination or Media Count : 78
Abstract : 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.
Descriptors : *GAS TURBINES, *FILM COOLING, *HEAT TRANSFER, *TURBULENT BOUNDARY LAYER, AIRFOILS, CASCADE STRUCTURES, CURVATURE, GAS TURBINE BLADES, MOMENTUM, WALLS, SURFACES
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE