| Citation: | ZHAO Yong, HU Jun. Analysis of the influence of inlet flow distortion on the off-design performance of fan/booster[J]. Journal of Aerospace Power, 2007, 22(7): 1087-1092. |
| [1] |
Robbins W H,Dugan J F.Prediction of off-design performance of multistage compressors[R].NASA SP-36,Chapter X,1965:297-310.
|
| [2] |
周燕佩,徐力平.计算流体动力学在航空叶轮机械中的应用一现状和展望[C]//21世纪航空动力发展研讨会.北京:中国航空动力专业分会,2000:100-104.
|
| [3] |
Johnsen I A,Bullock R O,Aerodynamic design of axialflow compressor[R].NASA SP-36.1965.
|
| [4] |
胡骏.均匀与非均匀进气条件下多级轴流压气机性能计算-均匀进气及径向畸变的影响[J].航空动力学报,2000,15(3):225-228.HU Jun.Calculation of off design performance of multistage compressors with uniform and radial distorted Inlet flow[J].Journal of Aerospace Power,2000,15(3):225-228.
|
| [5] |
燃气涡轮发动机进口流场畸变评审方法[R].北京:航空航天工业部301研究所,1989.
|
| [6] |
Gas turbine engine inlet flow distortion guideline[R].Society of Automotive Engineers,Inc,ARP-1420,March 1978.
|
| [7] |
Inlet total pressure distortion considerations for gas turbine engines[R].Society of Automotive Engineers,Ine.,AIR-1419,MAY 1983.
|
| [8] |
Miller G R.Shock losses in transonic compressor blade rows[J].ASME Journal of Engineering for Power,1961,83:235-242.
|
| [9] |
Bloch G S,Copenhaver W W,O'Brien W F.A shock loss model for supersonic compressor cascade[J].ASME Journal of Turbomachinery,1999,121(1):28-35.
|
| [10] |
Bloch G S,Copenhaver W W,O'Brien W F.Development of an off-design loss model for transonic compressor design[C]//Loss Mechanisms and Unsteady Flows in Turbomachines,AGARD-CP-571,Neuilly Sur Seine,France,NATO Research and Technology Organization,1996:16-1-16-14.
|
| [11] |
Boyer K M,O'Brien W F.An improved streamline curvature approach for off-design analysis of transonic axial compression systems[J].ASME Journal of Turbomachinery,2003,125(3):475-481.
|
| [12] |
赵勇,胡骏,郑大勇.用双激波模型计算风扇/压气机非设计点的性能[J].南京航空航天大学学报,2006,38(5):545-550.ZHAO Yong,HU Jun,ZHENG Dayong.Dual-shock loss model for off-design performance calculation of fan/compressor[J].Journal of Nanjing University of Aeronautics & Astronautics,2006,38(5):545-550.
|
| [13] |
胡骏.均匀与非均匀进气条件下多级轴流压气机性能计算-周向畸变的影响[J].航空动力学报,2000,15(3):229-232.HU Jun.Calculation of off-design performance of multistage compressor with circumferential distorted Inlet flow[J].Journal of Aerospace Power,2000,15(3):229-232.
|