期刊文献+

轴流式压气机喘振特性的某些规律 被引量:1

Some Research Findings Concerning the Surge Characteristics of Axial Compressors
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摘要 综合了几型压气机的试验结果,总结出喘振边界的某些规律。利用这些规律不仅可以减少试验的次数。还可以计算出喘振边界上有关的参数。 he author has summed un the experimental test results of several types of compressors, presenting some research findings concerning surge boundaties. The use of these findings can not only be conducive to reducing the number of times of tests but also serves a useful purpose during the calculation of the related parameters on surge boundaries.
作者 邬扬杰
出处 《热能动力工程》 CAS CSCD 北大核心 1994年第3期143-145,共3页 Journal of Engineering for Thermal Energy and Power
关键词 压气机 喘振特性 compressor,surge characteristics
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同被引文献6

  • 1程荣辉,雷丕霓,刘波,周拜豪,周盛.一种工程实用的多级轴流压气机特性二维数值计算方法[J].航空动力学报,2007,22(6):955-960. 被引量:13
  • 2Steinke R J.A Compute Code For Predicting Multi-stage AxialFlow Compressor Performance by a Meanline Stage Stacking Method[R].NASA TP -2020,1982.
  • 3Novak B A.Flow Field and Performance Map Computations for Axial -Flow Compressors and Turbines[R].AGABD Lecture Series,1976,83(5):1 -27.
  • 4Denton J D.The Use of a Distributed Body Force to Simulate Viscous Effects in 3D Flow Calculations[R].ASME 86-GT-144.1986.
  • 5Davis R L,Yao Jixian.Prediction of Compressor Stage Performance From Choke Through Stall[J].Journal of Propulsion and Power,2006,22 (3):550-557.
  • 6航空发动机设计手册总编委会.航空发动机设计手册:第8册-压气机[K].北京:航空工业出版社,2001.

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