Numerical investigation of impingement and heat transfer on inner surface of airfoil former cavity with film holes

[1] Schabacker J,Boles A,Johnson B V.PIV investigation of the flow characteristics in an internal coolant passange with 45° rib arrangement.ASME Paper No.99-GT-120,1999 [2] Liou T M,Wu Y Y.LDV measurements of periodic fully developed main and secondary flows in a channel with rib-disturbed walls[J].Journal of Fluids Engineering,1993,115:109-114 [3] 刘传凯,陶智,丁水汀,等.3种转角下旋转U形方通道的局部换热[J].北京航空航天大学学报,2006,32(3):284-287 Liu Chuankai,Tao Zhi,Ding Shuiting,et al.Local heat transfer in a rotating U-shaped square channel with three channel orientations[J].Journal of Beijing University of Aeronautics and Astronautics,2006,32(3):284-287(in Chinese) [4] Metzger D E,Bunker R S.Local heat transfer in internally cooled turbine airfoil leading edge regions:part 11—impingement cooling with film coolant extraction[J].Journal of Turbomachinery,1990,112:459-466 [5] Taslim M E,Setayeshgar L,Spring S D.An experimental evaluation of advanced leading edge impingement cooling concepts[J].Journal of Turbomachinery,2001,123:147-153 [6] Taslim M E,Pan Y,Spring S D.An experimental study of impingement on roughened airfoil leading-edge walls with film holes[J].Journal of Transactions,2001,123:766-773 [7] Taslim M E,Khanicheh A.Experimental and numerical study of impingement on an airfoil leading edge with and without showerhead and gill film holes[J].Journal of Transactions,2006,128:310-320 [8] Rama Kumar B V N ,Prasad B V S S S.Experimental investigation of flow and heat transfer for single and multiple rows of circular jets impinging on a concave surface.ASME GT 2008-51044,2008 [9] Alvarez J J,de la Calzada P,Krulic G.Heat transfer and flow characteristics of a leading edge impingement cooling system for low pressure turbine vanes.ASME GT 2008-50142,2008 [10] Taslim M E,Bethka D.Experimental and numerical impingement heat transfer in an airfoil leading-edge cooling channel with cross-flow[J].Journal of Turbomachinery,2009,131:011021.1-7 [11] 王开,徐国强,孙纪宁,等.冲击与气膜的组合形式对冷却效果的影响[J].北京航空航天大学学报,2008,34(7):751-754 Wang Kai,Xu Guoqiang,Sun Jining,et al.Effect of combined impingement cooling and fi1m cooling on hybrid cooling effectiveness[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(7):751-754( in Chinese) [12] 杨世铭,陶文铨.传热学[M].3版.北京:高等教育出版社,1998:165-166 Yang Shiming,Tao Wenquan.Heat transfer[M].3ed.Beijing:Higher Education Press,1998:165-166(in Chinese)