Volume 29 Issue 3
Mar.  2014
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DING Yang, CHANG Hai-ping, DU Zhi-neng. Cooling characteristics of full coverage film holes with opposite lateral ejection angles[J]. Journal of Aerospace Power, 2014, 29(3): 511-518. doi: 10.13224/j.cnki.jasp.2014.03.005
Citation: DING Yang, CHANG Hai-ping, DU Zhi-neng. Cooling characteristics of full coverage film holes with opposite lateral ejection angles[J]. Journal of Aerospace Power, 2014, 29(3): 511-518. doi: 10.13224/j.cnki.jasp.2014.03.005

Cooling characteristics of full coverage film holes with opposite lateral ejection angles

doi: 10.13224/j.cnki.jasp.2014.03.005
  • Received Date: 2013-01-06
  • Publish Date: 2014-03-28
  • Numerical investigations were performed to study the full coverage film cooling structure on the flow field characteristics, wall surface heat transfer coefficient, adiabatic wall film cooling effectiveness and integrated cooling effectiveness under consideration of heat conduction. Results indicates that kidney vortex pair generated in the flow field of film cooling with opposite lateral ejection angles makes the film spread wider laterally. Despite of raised heat transfer in this condition, the integrated cooling effectiveness increases as high adiabatic wall cooling effectiveness reduces the heat conduction. Under blowing ratio of 1.0, the slant hole with opposite lateral ejection angle of 45° has the highest integrated cooling effectiveness. The integrated cooling effectiveness of slant hole with opposite lateral ejection angle of 30° is the highest when blowing ratio of 1.5 and 2.0. Compared with corresponding slant hole with single lateral ejection angle, the film cooling with opposite lateral ejection angle of 15° has lower integrated cooling effectiveness. The cooling effectiveness of slant hole with opposite lateral ejection angles of 45° and 60° respectively are both comparable to the integrated cooling effectiveness of the corresponding structures with single lateral ejection angle. When compared with slant hole with single lateral ejection angle of 30°, the film cooling with opposite lateral ejection angle of 30° has higher integrated cooling effectiveness.

     

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  • [1]
    Mayle R E,Camarata F J.Multihole cooling film effectiveness and heat transfer[R].Journal of Heat Transfer,1975,97(2):534-538.
    [2]
    Sasaki M,Takahara K,Kumagai T,et al,Film cooling effectiveness for injection from multirow holes[R].ASME Paper 78-GT-32,1978.
    [3]
    Andrews G E,Khalifa I M,Asere A A,et al.Full coverage effusion film cooling with inclined holes[R].ASME Paper 95-GT-274,1995.
    [4]
    Fric T,Campbell R,Rettig M.Quantitative visualization of full coverage discrete hole film cooling[R].ASME Paper 97-GT-328,1997.
    [5]
    Lin Y Z,Song B,Li B,et al.Investigation of film cooling effectiveness of full-coverage inclined multihole walls with different hole arrangements[J].ASME Paper 2003-GT-38881,2003.
    [6]
    林宇震,宋波,李彬,不同倾斜角多斜孔壁冷却方式绝热温比研究[J].航空学报,1999,20(3):201-204. LIN Yuzhen,SONG Bo,LI Bin.Investigation of adiabatic wall effectiveness of the inclined multihole wall film cooling with different angles to the wall surface[J].Acta Aeronautica et Astronautica Sinica,1999,20(3):201-204.(in Chinese).
    [7]
    吴伟民,张青藩,李亚峰.全离散孔气膜冷却实验研究[J].航空动力学报,1994,9(4):387-390. WU Weimin,ZHANG Qingfan,LI Yafeng.Experimental investigation on full coverage discrete hole film cooling[J].Journal of Aerospace Power,1994,9(4):387-390.(in Chinese).
    [8]
    胡娅萍,吉洪湖.孔阵排列疏密度对致密多孔壁冷却效果的影响[J].推进技术,2005,26(1):28-33. HU Yaping,JI Honghu.Effect of porosity of holes array on cooling effectiveness of effusion cooling[J].Journal of Propulsion Technology,2005,26(1):28-33.(in Chinese).
    [9]
    杨卫华,王立,宋双文,等.冲击发散冷却流场结构PIV测量[J].航空动力学报,2010,25(3):483-487. YANG Weihua,WANG Li,SONG Shuangwen,et al.PIV measurement of flowfield for impingement effusion cooling[J].Journal of Aerospace Power,2010,25(3):483-487.(in Chinese).
    [10]
    胡娅萍,吉洪湖.致密多孔壁冷流入射角对冷却效果影响的数值研究[J].航空动力学报,2005,20(2):116-119. HU Yaping,JI Honghu.Numerical study of the blowing angle effectiveness on effusion cooling effectiveness[J].Journal of Aerospace Power,2005,20(2):116-119.(in Chinese).
    [11]
    杨成风,张靖周,杨卫华.全覆盖气膜孔阵列方式对冷却特性的影响[J].航空动力学报,2010,25(7):1524-1529. YANG Chengfeng,ZHANG Jingzhou,YANG Weihua.Effect of the holes array arrangement on the full coverage film cooling characteristics[J].Journal of Aerospace Power,2010,25(7):1524-1529.(in Chinese).
    [12]
    Sugimoto T,Tanaka R,Tsuji K,et al.Double jet film cooling structure:United States,US 7,682,132 B2[R].2010-05-23.
    [13]
    Kusterer K,Bohn D,Sugimoto T,et al.Double-jet ejection of cooling air for improved film-cooling[R].ASME Paper GT-2006-90854,2006.
    [14]
    Kusterer K,Bohn D,Sugimoto T,et al.Influence of blowing ratio on the double-jet ejection of cooling air[R].ASME Paper GT-2007-27301,2007.
    [15]
    Kusterer K,Elyas A,Bohn D,et al.Double-jet film-cooling for highly efficient film-cooling with low blowing ratios[R].ASME Paper GT2008-50073,2008.
    [16]
    Kusterer K,Elyas A,Bohn D,et al.A parametric study on the influence of the lateral ejection angle of double-jet holes on the film cooling effectiveness for high blowing ratios[R].ASME Paper GT2009-59321,2009.
    [17]
    王文三,唐菲,赵庆军,等.新型双射流冷却孔对气膜冷却效率影响的研究[J].工程热物理学报,2011,32(8):1291-1294. WANG Wensan,TANG Fei,ZHAO Qingjun,et al.An investigation of the effect of new-type double-jet film cooling(DJFC) hole on film cooling effectiveness[J].Journal of Engineering Thermophysics,2011,32(8):1291-1294.(in Chinese)
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