ZHANG Hong-xin , LI Yan-fei , CHEN Shao-wen , WANG Song-tao , WANG Zhong-qi . Effect of non-axisymmetric endwall modeling method on turbine blade performance under design conditions[J]. Journal of Dalian Maritime University, 2019 , 45(1) : 96 -101 . DOI: 10.16411/j.cnki.issn1006-7736.2019.01.012

[1]Hartland J C, Gregory- Smith D G, Harvey N W, et al.non-axisymmetric turbine end wall design: Part II: Experimental validation[R]. ASME 99-GT-338.
[2]Brennan G, Harvey H W, Rose M G, et al.Improving the efficiency of the Trent 500 HP turbine using Non-axisymmetric end wall: Part I: Turbine Design[R]. ASME 2001-GT-0444.
[3]Rose M G, Harvey N W, Seaman P.Improving the efficiency of the Trent 500 HP turbine using Non- axisymmetric end wall: Part II: Experimental validation[R]. ASME 2001-GT-0505.
[4]Praisner T J, Alley Bradley E, Grover E A, et al.Application of non-axisymmetric end wall contouring to Conventional and High-lift Turbine Airfoils[R]. ASME 2007-GT-27579.
[5]Bao Q N, Kyle D S.A simple procedure to reduce secondary flow effect in turbine nozzle guide vanes[R]. ASME 2007-GT-28159.
[6]Sonoda T, Hasenj?ger M，Arima T, et al.Effect of end wall contouring on performance of ultra-low aspect ratio transonic turbine inlet guide vanes[R]. ASME 2007- GT-28210.
[7] Ingram G L.End wall profiling for the reduction of secondary flow in turbines[D].Durham：Durham University, 2003.
[8]蒋演明.具有非对称端壁的涡轮叶栅气膜冷却数值研究[D]. 哈尔滨：哈尔滨工业大学硕士学位论文, 2008.
[9]JIANG Yan-ming.Numerical simulation of film cooling in turbine cascade with non-axisymmetric end wall method [D]. Harbin:Harbin Institute of Technology, 2008.(in Chinese)
[10]王睿.非对称端壁对扩压叶栅性能影响的数值研究[D]. 哈尔滨：哈尔滨工业大学硕士学位论文, 2012.
[11]WANG Rui.Numerical investigation effect of applying non-axisymmetric end wall on compressor cascade performance[D]. Harbin:Harbin Institute of Technology, 2012.(in Chinese).
[12]郑金, 李国君, 贾海东, 等.变工况下非轴对称端壁环形叶栅流场特性实验[J].航空动力学报, 2009, 23(12):2308-2313
[13]ZHENG Jin, LI Guo-jun, JIA Hai-dong, et al.Experimental investigation on flowfields of non-axisymmetric end wall of annular cascades in multi condition[J].Journal of Aerospace power, 2009, 23(12):2308-2313
[14]高增珣, 高学林, 袁新.透平叶栅非轴对称端壁的气动最优化设计[J].工程热物理学报, 2007, 28(4):589-591
[15]GAO Zeng-Xun, GAO Xue-Lin, YUAN Xin.Aerodynamic optimal design of non-axisymmetric end wall for a turbine cascade[J].Journal of engineering thermophysics, 2007, 28(4):589-591
[16]李国君, 马晓永, 李 军.非轴对称端壁成型及其对叶栅损失影响的数值研究[J].西安交通大学学报.[J].西安交通大学学报, 2005, 39(11):1169-1172
[17]LI Guo-jun, MA Xiao-yong, LI Jun.Non-axisymmetric turbine endwall profiling and numerical investigation of its effect on the turbine cascade loss[J]. Journal of Xi’an Jiao Tong University, 2005, 39(11).[J].Journal of Xi’an Jiao Tong University, 2005, 39(11):1169-1172
[18]赵刚剑, 刘波, 那振喆, 曹志远.采用新型非轴对称端壁优化设计方法提高涡轮性能的数值研究[J]. [J].推进技术, 2014, 35(5):597-602
[19]ZHAO Gang-jian, LIU Bo, NA Zhen-zhe, CAO Zhi-yuan.Improving the performance of turbine based on a new optimization design method[J]. [J].Journal of Propulsion Technology, 2014, 35(5):597-602
[20]Schwab S, Wendland D, Wirsum M.Numerical and Experimental investigation of tangential endwall contoured Blades in a 2-Stage Turbine[C].ASME Paper 2013-GT-94169. 2013
[21]温风波, 崔涛, 刘轶, 等.高压涡轮采用非轴对称端壁的研究[J].节能技术, 2013, 30(6):489-492
[22]WEN Feng-bo, CUI Tao, LIU Yi, et al.Research of Non-axisymmetric endwall application on high pressure turbine[J].Energy conservation technology, 2013, 30(6):489-492