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


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a195165.pdf


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