Experimental and numerical study on the effects of shaped multi-holes on the effectiveness of film cooling

被引:0
作者
Yaser Taheri
Mehran Rajabi Zargarabadi
Mehdi Jahromi
机构
[1] Semnan University,Department of Mechanical Engineering
[2] Malek Ashtar University of Technology,undefined
来源
Journal of Thermal Analysis and Calorimetry | 2021年 / 146卷
关键词
Experimental study; Film cooling; Multi-holes; Adiabatic effectiveness;
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暂无
中图分类号
学科分类号
摘要
In the present work, experimental and numerical study has been performed to investigate the effects of a novel film-cooling design with shaped multi-holes on the film-cooling effectiveness over a flat plate. A single cylindrical hole with 11.1 mm diameter has been replaced by multi-holes (14 holes with 2.97 mm diameter) with elliptical and fan-shaped configurations. The exit area, length to diameter ratio (L/D = 4.0) and injection angle (35°) of multi-holes are selected identical to the single cylindrical hole. The multi-holes were machined with a fixed spacing pitch (33.3 mm) between the centers of two adjacent holes. The surface temperature of the test plate was measured by an infrared camera. The experimental studies were performed at blowing ratios of 0.5 and 2. The numerical results based on the steady RANS with realizable k–ε turbulence model and enhanced wall treatment were capable to predict the influence of the shape of multi-hole configurations on overall adiabatic film-cooling effectiveness. The experimental and numerical results showed that replacing a single hole with a shaped multi-hole leads to a considerable increase in film-cooling effectiveness in both axial and lateral directions. According to the results at blowing ratio of 2.0, the elliptical and fan-shaped configurations provide a higher area-averaged film-cooling effectiveness by 75% and 248.2% in comparison with the single hole, respectively.
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页码:1723 / 1733
页数:10
相关论文
共 91 条
[1]  
Hale CA(2000)Film cooling effectiveness for short film cooling holes fed by a narrow plenum J Turbomach 122 553-557
[2]  
Plesniak MW(1999)Influence of the hole length-to-diameter ratio on film cooling with cylindrical holes J Turbomach 121 209-216
[3]  
Ramadhyani S(2003)Film cooling characteristics of a single round hole at various streamwise angles in a crossflow: part 1 effectiveness Int J Heat Mass Transf 46 221-235
[4]  
Lutum E(2001)Effect of compound angle injection on flat surface film cooling with large streamwise injection angle Exp Therm Fluid Sci 25 23-29
[5]  
Johnson BV(2013)Internal wall-jet film cooling with compound angle cylindrical holes Energy Convers Manag 68 54-62
[6]  
Yuen CHN(2006)Numerical approach to hole shape effect on film cooling effectiveness over flat plate including internal impingement cooling chamber Int J Heat Mass Transf 49 919-938
[7]  
Martinez-Botas RF(2020)Effect of mist concentration on the cooling effectiveness of a diffused hole mist cooling system J Therm Anal Calorim 127 718-725
[8]  
Nasir H(2005)Effect of hole geometry on the thermal performance of fan-shaped film cooling holes J Turbomach 25 282-300
[9]  
Ekkad SV(2012)Experimental and numerical study of film cooling with internal coolant cross-flow effects Exp Heat Transf 96 12-19
[10]  
Acharya S(2018)Investigation of boundary layer thickness and turbulence intensity on film cooling with a fan-shaped hole by direct numerical simulation Int Commun Heat Mass Transf 53 2996-3005