XU Wen-feng , SUN Peng , HUANG Long-sheng . Influence of stator tip clearance on compressor flow structure under near stall condition[J]. Journal of Dalian Maritime University, 2018 , 44(4) : 74 -82 . DOI: 10.16411/j.cnki.issn1006-7736.2018.04.012

[1]徐文峰, 孙鹏, 钟兢军.静叶叶顶部分间隙高度对压气机性能影响的数值研究[J].大连海事大学学报, 2017, 43(03):63-70 [2]Xu Wen-feng, Sun Peng, Zhong Jing-jun.Numerical study for the influence of stator tip clearance height on compressor performance[J].Journal of Dalian Maritime University, 2017, 43(03):63-70 [3]王掩刚, 牛楠, 赵龙波等.端壁抽吸位置对压气机叶栅角区分离控制的影响[J].推进技术, 2010, 31(4):433-437 [4]Wang Yan-gang, Niu Nan, Zhao Long-bo, et al.Effect on corner separation control for high load compressor cascade with different end-wall BLS position[J].Journal of Propulsion Technology, 2010, 31(4):433-437 [5]Joslyn H D.Dring R P[J].ASME Journal of Engineering for Gas Turbines and Power, 1985, 107(1):485-492 [6]肖文富，申晓霞，屈霁云等.轮毂造型抑制角区失速的数值研究[J].应用科学, 2010, 1(1):116-117 [7]Xiao Wen-fu, Sheng Xiao-xia, Qu Ji-yun, et al.Numerical investigation of stall in wheel shape control[J[J].Journal of Applied Science, 2010, 116-117., 2010, 1(1):116-117 [8]李秋实, 杨春, 肖文富等.端壁造型技术抑制角区失速的数值研究[J].自然科学进展, 2009, 19(5):537-543 [9]Li Qiu-shi, Yang Chun, Xiao Wen-Fu, et al.Numerical study of end wall modeling to suppress corner stall[J].Journal of Advances in Natural Science, 2009, 19(5):537-543 [10]周敏, 王如根, 曹朝辉等.开槽处理技术对叶片尾缘气流流动特性的影响[J].航空动力学报, 2009, 22(7):1100-1105 [11]Zhou Min, Wang Ru-gen, Chao Zhao-hui, et al.Influence of slot treatment on flow performance of blade trailing edge[J].Journal of Aerospace Power, 2009, 22(7):1100-1105 [12]Stephane Burguburu, Clement Toussaint.Numerical optimization of turbo-machinery blade[J].Journal of Turbo-machinery, ASME, 2004, 126(1):91-100 [13]Denton J D.The effects of lean and sweep on transonic fan performance: A computational study[J].Journal of Task Quart, 2002, 6(1):1-17 [14]毛明明, 宋彦萍, 王仲奇.跨声速轴流压气机动叶弯和掠效应的应用[J].工程热物理学报, 2009, 30(4):581-586 [15]Mao Ming-ming, Song Yan-ping, Wang Zhong-qi.Application of bowed and swept rotors a transonic axial compressor[J].Journal of Engineering Thermophysics, 2009, 30(4):581-586 [16]钟兢军, 韩少冰, 陆华伟.叶尖小翼对扩压叶栅气动特性影响的数值研究[J].工程热物理学报, 2010, 2(3):243-246 [17]Zhong Jing-jun, Han Shao-bing, Lu Hua-wei.Numerical simulation of blade tip winglet on the aerodynamic performance of compressor cascade2010,(02):243-246.[J].Journal of Engineering Thermophysics, 2010, 2(3):243-246 [18]Day I J.Aetive suppression of rotating stall and surge in axial compressors[J].ASME Journal of Turbomachinery, 1993, 115(1):40-47 [19]Suder K L, Hathaway M D, Thorp S A, et al.Compressor stability enhancement using discrete tip injection[J][J].ASME Journal of Turbomachinery, 2009, 123(1):14-23 [20]左志涛, 朱阳历, 张冬阳等.静叶轮毂间隙对高压压气机气动性能的影响[J].推进技术, 2013, 32(3):329-333 [21]ZUO Zhi-tao, ZHU Yang-li, ZHANG Dong-yang, et al.Numerical investigation of the stator hub gap effects on aerodynamic performance of a high-pressure compressor[J].Journal of Propulsion Technology, 2013, 32(3):329-333 [22]钟兢军.弯扭叶片控制扩压叶栅二次流动的实验研究[D]. 哈尔滨工业大学, 1995. [23]ZHONG Jing-jun.An experimental investigation by using curved blade to control secondary flow in compressor cascade[D]. Harbin Institute of Technology, 1995.(in Chinese) [24]韩少冰.叶尖小翼控制压气机叶顶间隙流动的研究[D]. 大连海事大学, 2013. [25]Han Shao-bing.Experimental and numerical investigation of compressor tip clearance flow control using blade tip winglet[D]. Dalian Maritime University, 2013.