| Citation: | SHI Lei, LIU Bo, ZHANG Peng, LI Jun, WANG Lei. One-dimensional characteristic optimization design for ten-stage high pressure compressor in commercial engine[J]. Journal of Aerospace Power, 2013, 28(7): 1564-1569.
|
| [1] |
Johnson M.One-dimensional,stage-by-stage,axial compressor performance model [R].ASME Paper 1991-GT-192,1991.
|
| [2] |
舒士甄,朱力,柯玄龄,等.叶轮机械原理[M].北京:清华大学出版社,1991.
|
| [3] |
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.(in Chinese)
|
| [4] |
李立君,黄杰,唐狄毅,等.轴流压气机特性预测[J].西北工业大学学报,2003,21(1):71-73. LI Lijun,HUANG Jie,TANG Diyi,et al.An accurate method for predicting performance characterictics of multi-stage axial compressor[J].Journal of Northwestern Polythchnical University,2003,21(1):71-73.(in Chinese)
|
| [5] |
陈江,刘太秋,李孝堂,等.五级轴流压气机气动设计数值研究[J].工程热物理学报,2010,31(6):943-946. CHEN Jiang,LIU Taiqiu,LI Xiaotang,et al.Aerodynamic design of five stage axial compressor by numerical simulation[J].Journal of Engineering Thermophysics,2010,31(6):943-946.(in Chinese)
|
| [6] |
李志刚,陶增元,丁康乐,等.一种改进的变几何压气机特性计算方法[J].航空发动机,2004,30(4):7-9. LI Zhigang,TAO Zengyuan,DING Kangle,et al.Simulation of variable geometry compressor characterictics[J].Aeroengine,2004,30(4):7-9.(in Chinese)
|
| [7] |
唐狄毅,宋文艳.压气机总特性与级特性相关性研究 [D].西安:西北工业大学,2001. TANG Diyi,SONG Wenyan.Research in the relation between total compressor characteristic and single-stage characteristic [D].Xi'an:Northwestern Polytechnical University,2001.(in Chinese)
|
| [8] |
张琛,詹志辉.遗传算法选择策略比较[J].计算机工程与设计,2009,30(23):5471-5478. ZHANG Chen,ZHAN Zhihui.Comparison of selection strategy in genetic algorithm[J].Computer Engineering and Design,2009,30(23):5471-5478.(in Chinese)
|
| [9] |
Day I J,Freeman C.The unstable behavior of low and high-speed compressors[R].ASME Paper 1993-GT-26,1993.
|
| [10] |
Gresh M T.Compressor performance:selection,operation,and testing of axial and centrifugal compressor[M].Oxford:Butterworth-Heinemann,1991.
|
| [11] |
张健,任铭林.静叶角度调节对压气机性能影响的试验研究[J].航空动力学报,2000,15(1):27-30. ZHANG Jian,REN Minglin.Experimental investigation on effect of stator vane angle adjustment on compressor performance[J].Journal of Aerospace Power,2000,15(1):27-30.(in Chinese)
|
| [12] |
Steinke R J.Design of 9.271 pressure-ratio five-stage core compressor and overall performance for first three stages.NASA TP-3597,1986.
|
| [13] |
Sun J,Elder R L.Numerical optimization of a stator vane setting in multistage axial-flow compressors[J].Journal of Power and Energy:Part A,1998,212(4):247-259.
|
| [14] |
刘波,周新海,严汝群.轴流压气机可控扩散叶型的数值优化设计[J].航空动力学报,1991,6(1):9-12. LIU Bo,ZHOU Xinhai,YAN Ruqun.Numerical optimization program for designing controlled diffusion compressor blading[J].Journal of Aerospace Power,1991,6(1):9-12.(in Chinese)
|
| [15] |
姜斌,吴晓鹏,王松涛.压气机分层优化气动设计体系研究[J].热能动力工程,2009,24(6):719-724. JIANG Bin,WU Xiaopeng,WANG Songtao.A study of an aerodynamic design system for the layered optimization of a compressor[J].Journal of Engineering for Thermal Energy and Power,2009,24(6):719-724.(in Chinese)
|
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