期刊文献+

均匀与非均匀进气条件下多级轴流压气机性能计算 被引量:4

Calculation of Performance of a Multistage Compressor with/without Distorted Inlet Flow
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作者 赵勇 胡骏
出处 《航空发动机》 2003年第4期1-6,共6页 Aeroengine
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参考文献8

  • 1[1]Robbins W H, Dugan J F. "Prediction of off- design performance of multistage compressors. NASA SP- 36, 1965,Chapter X: 297~310.
  • 2[2]Creveling H F. Axial flow compressor computer program for calculation off - design performance. NASA CR - 72427,1968.
  • 3[3]Aerodynamic design of axial - flow compressors. NASA SP- 36, 1965.
  • 4[4]Koch C C. Stalling pressure rise capability of axial flow compressor Stages. Journal of Engineering for Power,1981, 103:645~656.
  • 5[5]Jahnen W. Untersuchung von stroemungsinstabilitaeten in einem mehrstufigen axialverdichter unter den einfluss von eintrittsstoerungen. universitaet der bundeswehr muenchen, Doctor Dissertation, 1998.
  • 6[6]Hu J, Peters T, Fottner L. Numerical simulation of flow instabilities in high speed multistage compressors. Journal of Thermal Sciences, 1999, 8(1) :23~31.
  • 7[7]Mazzawy R S. Multiple segment parallel compressor model for circumferential flow distortion. Journal of Engineering for Power, 1977:288 ~296.
  • 8[8]Wright P I, etc. An improved compressor performance prediction model. ImechE 1991, C423/028.

同被引文献18

  • 1李景银,刘立军,李超俊.轴流压气机特性计算模型的研究[J].机械工程学报,1997,33(2):66-71. 被引量:8
  • 2ROBBINS W H,DUGAN J F.Prediction of off-design performance of multistage compressors[R].NASA SP-36,1965.
  • 3JOHNSON M S.One-dimensional,stage-by-stage,axial compressor performance model[R].ASME Paper 91-GT-192,1991.
  • 4朱明善,刘颖,林兆庄,等.工程热力学[M].北京:清华大学出版社,1996.
  • 5WRIGHT P,MILLER D.An improved compressor performance prediction model[J].Proc Inst Mech Eng,1991,205:69-82.
  • 6BETTNER J L,SEHRA A K.High-efficiency axial compressor[R].EPRI Report AP-4943,1986.
  • 7W. H. Robbins, J. F. Dugan. Prediction of off-design performance of multistage compressors[R]. NASA SP - 36,1965. 297 -310.
  • 8J. L. Bettner, A. K. Sehra. High- efficiency axial compressor[ R]. EPRI Report AP -4943, prepared by Allison Gas Turbine Division. 1986.
  • 9P. Wright, D. Miller. An improved compressor performance prediction model[J]. Proe. Inst. Mech. Eng., 1991:69-82.
  • 10Robbins W H,Dugan J F.Prediction of off-design performance of multistage compressors[ R].NASA SP-36,1965:297-310.

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