[1] 钟兢军, 韩少冰. 融合式叶尖小翼对低速压气机转子气动性能的影响[J]. 推进技术, 2014, 35(6): 749-757. (ZHONG Jing-jun, HAN Shao-bing. Effects of Blended Tip Winglet on Aerodynamic Performance of a Low Speed Compressor Rotor[J]. Journal of Propulsion Technology, 2014, 35(6):749-757.)
[2] 李相君, 楚武利, 张皓光. 高负荷轴流压气机叶栅二次流动与损失关联性探讨[J]. 推进技术, 2014, 35(7): 914-925. (LI Xiang-jun, CHU Wu-li, ZHANG Hao-guang. Investigation on Relation Between Secondary Flow and Loss on a High Loaded Axial-Flow Compressor Cascade[J]. Journal of Propulsion Technology, 2014, 35(7): 914-925.)
[3] 钟兢军, 苏杰先, 王仲奇. 压气机叶栅中应用弯曲叶片的研究[J]. 航空动力学报, 1998, 13(1): 7-12.
[4] Gümmer V, Wenger U, Kau H P. Using Sweep and Dihedral to Control Three-Dimensional Flow in Transonic Stators of Axial Compressors[J]. Journal of Turbomachinery, 2001, 123(1): 40-48.
[5] Howell A R. Fluid Dynamics of Axial Compressors[J]. Proceedings of the Institution of Mechanical Engineers, 1945, 153(1): 441-452.
[6] Lu J, Chu W, Wu Y. Effects of Endwall Profiling on Axial Flow Compressor Stage[R]. ASME 2009-GT -59418.
[7] 杜鑫, 焦映厚, 张龙新, 等. 端弯控制扩压叶栅角区分离的机制分析[J]. 中国机电工程学报, 2014, 34(2): 309-314.
[8] Hergt A, Meyer R, Engel K. Effects of Vortex Generator Application on the Performance of a Compressor Cascade[J]. Journal of Turbomachinery, 2013, 135(2): 1-10.
[9] Hoeger M, Cardamone P, Fottner L. Influence of Endwall Contouring on the Transonic Flow in a Compressor Blade[R]. ASME 2002- GT-30440.
[10] Kro?ger G, Cornelius C, Nicke E. Rotor Casing Contouring in High Pressure Stages of Heavy Duty Gas Turbine Compressors with Large Tip Clearance Heights[R]. ASME 2009-GT -59626.
[11] Ito Y, Watanabe T, Himeno T. Effects of Endwall Contouring on Flow Instability of Transonic Compressor[J]. International Journal of Gas Turbine, Propulsion and Power Systems, 2008, 2(1): 24-29.
[12] 杨春, 李秋实, 袁巍, 等. 轮毂修型对压气机静子角区堵塞的影响[J]. 航空动力学报, 2009, 10(24): 2333-2337.
[13] Du X, Wang S T, Wang Z Q. Study on the Effect of End-Bend Cantilevered Stator in a 2-Stage Axial Compressor[J]. Journal of Thermal and Science, 2009, 18(2): 119-125.
[14] 徐全勇, 侯安平, 李绍斌, 等. 轮毂曲线对跨声速压气机转子性能的影响[J]. 工程热物理学报, 2009, 30(5): 761-764.
[15] Pesteil A, Cellier D, Domercq O, et al. CREATE: Advanced CFD for HPC Performance Improvement[R]. ASME GT-2012-68844.
[16] Dorfner C, Hergt A, Nicke E, et al. Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part I: Principal Cascade Design and Compressor Application[J]. Journal of Turbomachinery, 2011, 133(2): 1-6.
[17] Hergt A, Dorfner C, Steinert W, et al. Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation[J]. Journal of Turbomachinery, 2011, 133(2): 1-8.(编辑:朱立影) * 收稿日期:2016-01-26;修订日期:2016-03-07。基金项目:国家自然科学基金(51436002;51206035);国家自然科学基金创新研究群体项目(51121004)。作者简介:张龙新,男,博士生,研究领域为高负荷压气机设计。E-mail: zlx_hit@hotmail.com
|