Comparisons of Overall Performance Among Double-Jet Film Cooling Holes, Cylinder Holes, and Fan-Shaped Holes

Author:

Lei Jiang1,Yao Jiaxu23,He Jianhong1,Yang Xi1,Zhang Ke1,Wright Lesley M.4

Affiliation:

1. State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi'an Jiaotong University , Xi'an, Shaanxi 710049, China

2. State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi'an Jiaotong University , Xi'an, Shaanxi 710049, China ; , Deyang, Sichuan 618000, China

3. State Key laboratory of Clean and Efficient Turbomachinery Power Equipment, Dongfang Electric Corporation Dongfang Turbine Co., Ltd. , Xi'an, Shaanxi 710049, China ; , Deyang, Sichuan 618000, China

4. Turbine Heat Transfer Laboratory, Department of Mechanical Engineering, Texas A&M University , College Station, TX 77843-3123

Abstract

Abstract In this paper, the film-cooling effectiveness (η) and heat transfer coefficient (h) of different film hole geometries are investigated, including double-jet film cooling (DJFC) holes, streamwise cylindrical holes, and fan-shaped holes, both experimentally and numerically. Results reveal that when the blowing ratio is less than 1.0, the DJFC holes have the highest η and the highest h, as well as the highest net heat flux reduction (NHFR). However, a higher blowing ratio (>1.0) leads to a quickly decreasing NHFR of DJFC holes. The asymmetric antikidney vortex and the high turbulent kinetic energy (TKE) are dominant in the performance of the DJFC holes. Owing to medium effectiveness and the lowest heat transfer coefficient, the fan-shaped holes possess the highest net heat flux reduction at M = 2.0 although the value is negative. The relatively weak kidney vortex and the low TKE can explain the phenomena. The cylindrical holes have the lowest η and the lowest NHFR due to the kidney vortex and relatively higher TKE.

Funder

National Natural Science Foundation of China

Publisher

ASME International

Reference32 articles.

1. A Detailed Analysis of Film-Cooling Physics: Part I-Streamwise Injection With Cylindrical Holes;ASME J. Turbomach.,2000

2. Film Cooling Following Injection Through Inclined Circular Tubes;Isr. J. Technol.,1970

3. Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio;ASME J. Turbomach.,1991

4. The Effect of Density Ratio on the Film-Cooling of a Flat Plate,1985

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