[1] Cesar Celis, Paula de M Ribeiro Pinto,Rafael S Barbosa, et al.Modeling of Variable Inlet Guide Vanes Affects on a One Shaft Industrial Gas Turbine Used in a Conbined Cycle Application [R].ASME 2008-GT-50076.
[2] George A Bobula, Ronald H Soeder,Leo A Burkard.Effect of Variable Guide Vanes on the Performance of a High-Bypass Turbofan Engine [J].Journal of Aircraft, 1983,0(4):306-311.
[3] Vahdati M, Sayma A I,Imregun M, et al.Multibladerow Forced Response Modeling in Axial-Flow Core Compressors [J].ASME,Journal of Turbomachinery, 2007,9(2):412-420.
[4] Semiu A Gbadebo,Nicholas A Cumpsty,Tom P Hynes.Three-Dimensional Separations in Axial Compressors [R].ASME 2004-GT-53617.
[5] Chi R M.Separated Flow Unsteady Aerodynamic Theory [J].Journal of Aircraft, 1985,2(11):956-964.
[6] Sbardella L,Imregun M.Linearized Unsteady Viscous Turbomachineary Flows using Hybrid Grids [J].ASME, Journal of Turbomachinery, 2001,3:568-582.
[7] Vahdati V, Simpson G, Imregun M.Unsteady Flow and Aerolasticity Behaviour of Aero-Engine Core Compressors During Rotating Stall and Surge [R].ASME 2006-GT-90308.
[8] Michael G List, Steven E Gorrell,Mark G Turner.Investigation of Loss Generation in an Embedded Transonic Fan Stage at Several Gaps Using High-Fidelity, Time-Accurate Computational Fluid Dynamics [J].ASME, Journal of Turbomachinery, 2007,2(1):011014-1-7.
[9] 张涵信.分离流和涡运动横截面流态的拓扑[J].空气动力学报, 1997,5(1):1-11.
[10] 张涵信.分离流与旋涡运动的结构分析[M].北京:国防工业出版社, 2005.
[11] Hans Martensson, Horgen Burman,Ulf Johansson.Design of the High Pressure Ratio Transonic1-1/2Stage Fan Demonstrator Hulda[R].ASME 2007-GT-27793.
[12] 张华良, 董学智, 谭春青, 等.扩压叶栅二维流动分离的数值模拟[J].工程热物理学报, 2008,9(8):1297-1300.
[13] 侯安平,周盛.对圆柱和二维叶栅在平面叶栅风洞中旋涡脱落的试验研究[J].空气动力学报, 2004,2(1):101-108.
[14] 王英锋, 胡骏, 李传鹏,等.上游转子对下游静子叶片气动力的影响[J].航空学报, 2006,7(4):545-550.
[15] Bo song, Wing F Ng.The Role of AVDR in Linear Cascade Testing [C].ISJPPE,2006:478-488.
[16] 王新月.气体动力学基础[M].西安:西北工业大学出版社, 2006.
|