Citation: | Numerical simulation of flat baffle inlet distortion coupled with compressor[J]. Journal of Aerospace Power, 2017, 32(3): 568-576. doi: 10.13224/j.cnki.jasp.2017.03.007 |
[1] |
Callanan G M,Stenning A H.Attenuation of inlet flow distortion upstream of axial flow compressors[J].Jounal of Aircraft,1971,8(4):227-233.
|
[2] |
ZHANG Jing,LIN Feng,CHEN Jing,et al.Effects of rotating inlet distortion on flow stability of an axial compressor[R].AIAA-2007-5062,2007.
|
[3] |
Mazzawy R S.Multiple segment parallel compressor model for circumferential flow distortion[J].Journal of Engineering for Power,1977,99(2):288-296.
|
[4] |
Hawthorne W R.Non-axisymmetric flow through annular actuator disks:inlet distortion problem[J].Journal of Engineering for Power,1978,100(4):604-617.
|
[5] |
Stenning A H.Inlet distortion effects in axial compressors[J].Journal of Fluids Engineering,1980,102(3):7-12.
|
[6] |
GONG Yifang.A computational model for rotating stall and inlet distortions in multistage compressors[D].Cambridge,US:Massachusetts Institute of Technology,1999.
|
[7] |
Chima R V.A three-dimensional unsteady CFD model of compressor stability[R].NASA TM-2006-214117,2006.
|
[8] |
郑宁,邹正平,徐力平.风扇进气畸变三维非定常数值模拟技术研究[J].航空动力学报,2007,22(1):60-65.ZHENG Ning,ZOU Zhengping,XU Liping.3D unsteady numerical simulation of fan/compressor with inlet distortion[J].Journal of Aerospace Power,2007,22(1):60-65.(in Chinese)
|
[9] |
刘永泉,刘火星,郑宁.某发动机风扇进气畸变数值模拟[J].航空动力学报,2012,27(9):2009-2015.LIU Yongquan,LIU Huoxing,ZHENG Ning.Numerical simulation of an aero-engine fan with inlet distortion[J].Journal of Aerospace Power,2012,27(9):2009-2015.(in Chinese)
|
[10] |
安玉戈,刘火星.压气机进气畸变数值模拟技术研究[J].航空学报,2012,33(9):1624-1632.AN Yuge,LIU Huoxing.Numerical simulation of compressor with inlet distortion[J].Acta Aeronautica et Astronautica Sinica,2012,33(9):1624-1632.(in Chinese)
|
[11] |
Xu L.Assessing viscous body forces for unsteady calculations[R].ASME Paper GT-2002-30329,2002.
|
[12] |
SUN Xiaofeng.Three-dimensional compressible flow stability theory of rotating stall[R].Beijing:Beijing University of Aeronautics and Astronautics BUAA Technical Report BH-B4765,1996.
|
[13] |
SUN Xiaofeng.On the relation between the inception of rotating stall and casing treatment[R].AIAA 96-2579,1996.
|
[14] |
SUN Xiaofeng,LIU Xiaohua,HOU Ruiwei.A general theory of flow instability inception in turbomachinery[R].AIAA Journal,2013,51(7):1675-1687.
|
[15] |
SUN Xiaofeng,SUN Dakun,YU Weiwei. A theory of compressor stability enhancement using novel casing treatment:Part Ⅰ methodology[J].Journal of Propulsion and Power,2015,30(5):1-12.
|
[16] |
Greitzer E M,Tan C S,Graf M.Internal flow concepts and applications[M].New York:Cambridge University Press,2004.
|
[17] |
Kiwada G.Development of a body force description for compressor stability assessment[D].Cambridge,US:Massachusetts Institute of Technology,2008.
|
[18] |
刘东健.轴流压气机端壁区域复杂流动特性的实验与仿真研究[D].西安:空军工程大学,2014.LIU Dongjian.Experimental and numerical simulation study on complex flow characteristics in axial-flow compressor casing[D].Xian,Air Force Engineering University,2014.(in Chinese)
|
[19] |
程邦勤,陶增元,李军.某型涡扇发动机进气总压畸变的试验研究[J].推进技术,2003,24(1):21-23.CHENG Bangqin,TAO Zengyuan,LI Jun.Aerodynamic stability analysis of inter total pressure distortion for turbofan[J].Journal of Propulsion Technology,2003,24(1):21-23.(in Chinese)
|