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
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE