期刊文献+

时间倾斜算子在离心压缩机动/静相干非定常模拟中的应用 被引量:3

APPLICATION OF THE TIME-INCLINED OPERATOR ON THE UNSTEADY NUMERICAL SIMULATION IN CENTRIFUGAL COMPERSSOR
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摘要 本文介绍了用时间倾斜算子来处理非定常计算中非等栅距的方法。通过引入时间倾斜算子对N-S方程进行转化,而不对几何结构作任何改变,且所计算的叶片通道数小,以确保有较好的计算效率。粘性的影响被归类到源项中来进行求解,在作时间倾斜的方程转换时,就不用忽略粘性应力项的影响,使得方程的求解更为真实。同商用软件的计算结果进行了比较,结果表明应用本文所发展的程序,能很好的预测离心压缩机级的非定常流动。 A numerical method for the calculation of unsteady stator/rotor interaction in turbomachinery stage of arbitrary pitch ratio using time-inclined operator is presented. It is developed on the basis of the program solving the three dimensional, viscous, steady flowfield in the centrifugal compressor. Dual time-stepping is adopted to realize the unsteady simulation; time-inclined operator is employed to transform the Navier-Stokes equations. It is realized without an approximation to a ratio of small integers or to scale geometry, the passages used for computation are minimum, and the computation time is also small. The results using time-inclined operator are also compared with the computation using NUMECA. It shows the program developed by the author can predict the flowfield in the centrifugal compressor accurately.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2005年第5期770-772,共3页 Journal of Engineering Thermophysics
基金 国家自然科学基金资助项目(No.50276047)
关键词 时间倾斜算子 非等栅距 非定常 双时间步 time-inclined operator arbitrary pitch unsteady dual time-stepping
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参考文献8

  • 1席光,党政,王尚锦.离心式动/静相干叶排内部非定常流动的数值计算[J].西安交通大学学报,2002,36(1):12-15. 被引量:8
  • 2Dawes W N. A Numerical Study of the Interaction of a Transonic Compressor Rotor Overtip Leakage Vortex with the Following Stator Blade Row. ASME 94-GT-156,1994.
  • 3Arnone A, Pacciani R. Rotor Stator Interaction Analysis Using the Navier-Stokes Equations and a Multigrid Method. ASME Journal of Turbomachinery, 1996, 118:679-689.
  • 4He L, Denton J D. Three-Dimensional Time-Marching Inviscid and Viscous Flow Solutions for Unsteady Flows Around Vibrating Cascades. ASME Journal of Turbomachinery, 116:469-476.
  • 5Giles M B. Stator/Rotor Interaction in a Transonic Turbine. AIAA Journal Propulsion and Power, 1990, 6(5):621-627.
  • 6Gao Limin, Xi Guang, Wang Shangjin. The Influence of Tip Clearance on the Flow Field and Aerodynamic Performance of the Centrifugal Impeller. Chinese Journal of Aeronautics, 2002, 15(3): 139-144.
  • 7Jung A R, Mayer J F, Stetter H. Simulation of 3-D Unsteady Stator/Rotor Interaction in Turbomachinery Stages of Arbitrary Pitch Ratio. ASME 96-GT-69, 1996.
  • 8Sleiman M. Simulation of 3-D Viscous Compressible Flow in Multistage Turbomachinery by Finite Element Mrthods: [Ph. D. Thesis]. Canada: Concordia University,1999.

二级参考文献1

  • 1党政.叶轮机械非等栅距动/静相干叶排内部非定常流动的数值分析[M].西安:西安交通大学能源与动力工程学院,2000..

共引文献7

同被引文献14

  • 1高丽敏,席光,周莉,王尚锦.级环境下叶片扩压器流场的实验与数值研究[J].力学学报,2005,37(1):110-119. 被引量:9
  • 2Erdos J I,Alzner E,McNally W.Numerical Solution of Periodic Transonic Flow Through A Fan Stage.AIAA Journal,1977,15(11):1559-1568
  • 3Rai M M,Madavan N K.Multi-airfoil Navier-Stoles Simulations of Turbine Rotor-Stator Interaction.Journal of Turbomachinery,1990,112:377-384
  • 4Giles M B.UNSFLO:A Numerical Method for the Calculation of Unsteady Flow in Turbomachinery.1991,GTL Rep.No.205,MIT Gas Turbine Laboratory
  • 5Dawes W N.A numerical study of the interaction of a transonic compressor rotor overtip leakage vortex with following stator blade row[R].ASME Paper 94-GT156,1994.
  • 6Arnone A,Pacciani R.Rotor-stator interaction analysis using the navier-stokes equations and a multigrid method[J].Journal of Turbomachinery,1996,118(4):679-689.
  • 7He L,Denton J D.Three-dimensional time-marching inviscid and viscous flow solutions for unsteady flows around vibrating cascades[J].Journal of Turbomachinery,1994,116(3):469-476.
  • 8Giles M.UNSFLO:a numerical method for the calculation of unsteady flow in turbomachinery[R].[S.l.]:MIT Gas Turbine Laboratory,GTL Report 205,1991.
  • 9Giles M B.Stator/rotor interaction in a transonic turbine[J].Journal Propulsion and Power,1990,6(5):621-627.
  • 10Laumert B.Simulation of rotor/stator interaction with a 4D finite volume method[R].ASME Paper GT-2002-30601,2002.

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二级引证文献2

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