Improvement of film cooling effectiveness with a small downstream block body

被引:7
作者
Khorsi, A. [1 ]
Guelailia, A. [1 ]
Hamidou, M. K. [1 ]
机构
[1] Univ Sci & Technol Oran Mohamed Boudiaf, Lab Appl Mech, BP 1505, El Mnaouer 31000, Oran, Algeria
关键词
film cooling; adiabatic effectiveness; compound angle; flat plate; finite volume method; COMPOUND ANGLE; HOLES; INJECTION;
D O I
10.1134/S0021894416040106
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The aim of this study is to predict the improvement in film cooling performance over a flat plate through a single row of cylindrical holes with different streamwise angles by using the Ansys CFX software package. In order to improve the film cooling effectiveness, a short crescent-shaped block is placed downstream of a cylindrical cooling hole. The numerical results of the cylindrical hole without the downstream short crescent-shaped block are compared with experimental data.
引用
收藏
页码:666 / 671
页数:6
相关论文
共 20 条
[1]  
An B., 2013, ASME PAPER, V135
[2]  
[Anonymous], GT200727528 ASME
[3]   Film cooling predictions of simple and compound angle injection from one and two staggered rows [J].
Azzi, A ;
Abidat, M ;
Jubran, BA .
NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2001, 40 (03) :273-294
[4]  
Bunker R. S., 2002, ASME Paper GT-2002-30178
[5]   EFFECT OF SURFACE-ROUGHNESS ON FILM COOLING PERFORMANCE [J].
GOLDSTEIN, RJ ;
ECKERT, ERG ;
CHIANG, HD ;
ELOVIC, E .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1985, 107 (01) :111-116
[6]   Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits [J].
Gritsch, M ;
Schulz, A ;
Wittig, S .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1998, 120 (03) :549-556
[7]  
Han J.-C., 2012, Gas turbine heat transfer and cooling technology
[8]   Adiabatic effectiveness, thermal fields, and velocity fields for film cooling with large angle injection [J].
Kohli, A ;
Bogard, DG .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1997, 119 (02) :352-358
[9]   2-EQUATION EDDY-VISCOSITY TURBULENCE MODELS FOR ENGINEERING APPLICATIONS [J].
MENTER, FR .
AIAA JOURNAL, 1994, 32 (08) :1598-1605
[10]  
Na S., 2006, P GT2006 ASME TURB E