期刊文献+

高速离心压缩机旋转失速的三维数值模拟 被引量:3

Three-dimensional numerical simulation for rotating stall inside high-speed centrifugal compressor
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摘要 使用商业计算流体力学软件CFX求解三维雷诺平均的Navier-Stokes方程组,结合出口气腔模型对某带无叶扩压器的离心压缩机的旋转失速现象进行数值模拟。首先使用定常计算得到了该离心压缩机的稳态性能曲线,并和实验测量值进行了比较。然后引入出口气腔模型,模拟离心压缩机内的旋转失速流动。在小流量下,从沿流线方向速度等值线图和径向速度等值线图中观察得到了离心压缩机内部流场的非定常流动现象。还研究了气腔模型不同参数对失速流动的影响,结果表明气腔体积越大,计算得到的失速频率越低。 Numerical simulation results of rotating stall flow phenomenon inside a centrifugal compressor with vaneless diffuser by solving three-dimensional Reynolds averaged compressible N-S equations using commerical CFD software CFX adopting RNG k-ε turbulence model are presented.Firstly,the steady performance curve is obtained using steady calculations and compared with experimental results.Secondly,a plenum chamber model is added at the vaneless diffuser outlet to simulate the rotating stall flow phenomenon inside the centrifugal compressor.This paper presents the centrifugal compressor internal flow fields at different times during the stall cycle at the least mass flow rate and the stall flow phenomenon has been observed.The Plenum chamber influence on the rotating stall is also investigated.The simulation indicates that the greater the plenum chamber volume,the lower the stall frequency.
出处 《推进技术》 EI CAS CSCD 北大核心 2007年第4期373-377,共5页 Journal of Propulsion Technology
关键词 压气机 旋转失速 气腔模型^+ Compressor Rotating stall Plenum chamber model^+
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参考文献13

  • 1蒋康涛,徐纲,黄伟光,陈静宜.低速轴流压气机旋转失速的二维数值模拟[J].工程热物理学报,2003,24(6):935-938. 被引量:7
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二级参考文献8

  • 1Nie C, Xu G, Cheng X, et al. Micro Air Injection and Its Unsteady Response in a Low-Speed Axial Compressor. J of Turbomachinery, 2002, 124(4): 572-579.
  • 2Outa E, Kato D, Chiba K. An N-S Simulation of Stall Cell Behavior in a 2-D Compressor Rotor-Stator System at Various Loads. ASME 94-GT-257, 1994.
  • 3Outa E, Ohta Y, Kato D, et al. Two Dimensional Study on Evolution of Deep Rotating Stall under Uniform Inlet Conditions in an Axial Compressor Cascades. ISABE 99-7219, 1999.
  • 4He L. Computational Study of Rotating Stall Inception in Axial Compressor. J of Propulsion and Power, 1997,13(1): 31-38.
  • 5Saxer Felici H M, Saxer A P, Inderbitzin A, et al. Prediction and Measurement of Rotating Stall Cells in an Axial Compressor. ASME 98-GT-67, 1998.
  • 6Saxer Felici H M, Saxer A P, Inderbitzin A, et al. Numerical and Experimental Study of Rotating Stall in an Axial Compressor Stage. AIAA 98-3298, 1998.
  • 7Saxer Felici H M, Saxer A P, Ginter F, et al. Sturcture and Propagation of Rotating Stall in a Single- and a Multi-Stage Axial Compressor. ASME 99-GT-452, 1999.
  • 8Nishizawa T, Takata H. Numerical Study on Rotating Stall in Finite Pitch Cascades. ASME 94-GT-258, 1994.

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