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畸变条件下跨声速轴流压气机内部流动分析 被引量:1

ANALYSIS OF THE INTERNAL FLOW IN A TRANSONIC AXIAL-FLOW COMPRESSOR UNDER INLET DISTORTION
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摘要 以某跨声速轴流压气机单转子为研究对象,应用数值模拟技术,采用全通道计算方案,利用Jameson有限体积中心差分格式并结合Spalart-Allmaras湍流模型获得进口畸变条件下该轴流压气机转子性能和内部流动细节,详细分析了进气周向总压畸变对压气机转子内流场流动结构的影响.并将计算结果与实验结果进行了比较,结果表明,数值模拟的结果与实验结果符合较好,计算方案切实可行. Under the inlet pressure distortion, the internal 3D viscous flow fields of the transonic axial-flow compressor is numerically analyzed using the full passage method, based on a finite volume method and the Spalaxt-Allmaras turbulent model. The performance for the compressor and the internal flow structure are analyzed in detail under the inlet distortion condition. Compared with experimental data, good agreements axe found, which indicates that the model and the method are practical and reliable.
出处 《力学与实践》 CSCD 北大核心 2009年第5期8-14,共7页 Mechanics in Engineering
关键词 轴流压气机 数值模拟 全通道 畸变 axial-flow compressor, numerical .simulation, full passage, distortion
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参考文献15

  • 1Mokelke H. The prediction of steady,circumferential pressure and tempe -rature distortions in multistage axial flow compressors. ASME Journal of Engineering for Power, 1980, 102:448-458.
  • 2Mazzawy RS. Modeling and analysis of the TF30-P-3 Compressor system with inlet pressure distortion. NASA CR - 134996, 1976.
  • 3Debogdan CE. Effect of a 180 extent inlet pressure distortion on the internal flow conditions of a TF30-P-3 engine. NASA TM X-3267, 1975.
  • 4Marshall JG. Prediction of low engine order inlet distortion driven response in a low aspect ratio fan. ASME Paper 2000- GT- 0374.
  • 5陈大光,张津,朱之丽.推重比15一级发动机有关总体性能的关键技术和难点分析[J].航空动力学报,2001,16(1):8-12. 被引量:16
  • 6Hail E J, Topp DA, Heigegger N J, et al. Endwall treatment inlet flow distortion analysis final report. NAS3-25270, 1996.
  • 7Denton JD. A time marching method for two-and three dimensional blade to blade row. ARC R&M 3775, 1974.
  • 8Denton JD, Singh UK. Time Marching Methods for Turbomachinery Flow Calculation, Von Karman Institute for Fluid Dynamics, Application of Numerical Methods to Flow Calculations in Turbomachines. 1979.
  • 9Denton JD. The calculation three-dimensional viscous flow through multistage turbomachines. ASME Journal of Turbomachinery, 1992, 114(2): 18-26.
  • 10Adamczyk JJ. Model Equation for Simulating Flows in Multistage Turbomachines, NASA TM-86869, 1985.

二级参考文献8

  • 1Oates G C 陈大光等(译).飞机推进系统技术与设计[M].北京:航空工业出版社,1992..
  • 2王立峰.战斗机过失速机动飞行条件下综合飞行/推进控制研究.北京航空航天大学博士学位论文[M].,2000..
  • 3邓学蓥 刘志伟.先进战斗机二元喷管矢量喷流的干扰效应研究.中国航空科技文献[M].,1992..
  • 4王立峰,博士学位论文,2000年
  • 5Peng J L,ASME Paper 2000-GT-0029,2000年
  • 6Mattern D L,AIAA 97-2902,1997年
  • 7邓学蓥,中国航空科技文献 HJB92 10 92,1992年
  • 8陈大光(译),飞机推进系统技术与设计,1992年

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