[1] |
Harry D P,Lubick R J.Inlet-air distortion effects on stall,surge and acceleration margin of a turbojet engine equipped with variable compressor inlet guide vanes[R].NACA RM E54K26,1955.
|
[2] |
Malker L,Curtis L,et al.Effects of unequal air-flow distribution from twin inlet ducts on performance of an axial-flow turbojet engine[R].NACA RM E54E13,1954.
|
[3] |
Hermanson K,Thole K.Effect of non-uniform inlet conditions on endwall secondary flow[J].Journal of Turbomachinery,2002,124(10):623-631.
|
[4] |
Hirai K,Kodama H,Nozaki O,et al.Unsteady three-dimensional analysis of inlet distortion in turbomachinery[R].AIAA 1997-2735,1997.
|
[5] |
Hah C,Rabe D,Sullivan T,et al.Effects of inlet distortion on the flow field in a transonic compressor rotor[J].ASME Journal,1998,120(2):233-246.
|
[6] |
Doyle M,Dixon S,Horlock J.Circumferential asymmetry in axia flow compressors[J].Journal of the Royal Aeronautical Soeiety,1966,70(10):956-963.
|
[7] |
Greitzer E.Surge and rotating stall in axial flow compressors:Part Ⅰ theoretical compression system model[J].Journal of Engineering for Power,1976,98(2):201-213.
|
[8] |
Stenning A H.Inlet distortion effects in axial compressors[J].Journal of Fluids Engineering,1980,102(1):7-13.
|
[9] |
Chue R,Hynes T,Greitzer E,et al.Calculation of inlet distortion induced compressor flow field instability[J].Journal of Heat and Fluid Flow,1989,10(3):211-223.
|
[10] |
张靖煊.畸变条件下轴流压气机叶顶间隙流对流动失稳影响的非定常机制[D].北京:中国科学院,2007. ZHANG Jingxuan.The unsteady mechanism and the role of tip clearance flow in distortion induced instability in an axial compressor[D].Beijing:Chinese Academy of Sciences,2007.(in Chinese)
|
[11] |
YAO Jixian,Steven E,Aspi R.High-fidelity numerical analysis of per-rev-type inlet distortion trasfer in mutistage fans:Part Ⅰ simulations with selected blade rows[R].ASME Paper GT-2008-50812,2008.
|
[12] |
YAO Jixian,Steven E,Aspi R.High-fidelity numerical analysis of per-rev-type inlet distortion trasfer in mutistage fans:part Ⅱ entire component simulation and investigation[R].ASME Paper GT-2008-50813,2008.
|
[13] |
赵勇.风扇/压气机非设计点性能计算和进气畸变影响预测方法研究[D].南京:南京航空航天大学,2008. ZHAO Yong.Investigations on off-design performance computation and predicting methods of inlet flow distortion for fan/compressor[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2008.(in Chinese)
|
[14] |
李茂义,陆亚钧,弓志强.进气畸变条件下轴流压转子内流的PIV研究[J].航空动力学报,2006,21(3):461-466. LI Maoyi,LU Yajun,GONG Zhiqiang.PIV investigation of the internal flow in an axial flow compressor rotor under inlet distortion[J].Journal of Aerospace Power,2006,21(3):461-466.(in Chinese)
|
[15] |
LI Maoyi,YUAN Wei,SONG Xizhen,et al.An experimental investigation about the effect of the partial treatment on a transonic axial-flow compressor performance under inlet distortion[R].ASME Paper GT-2012-68442,2012.
|