期刊文献+

无动量亏损尾迹三维数值模拟

Three-dimensional Numerical Simulation on Momentumless Wake
下载PDF
导出
摘要 利用计算流体力学软件,对粘性不可压缩流体的平板翼型绕流进行了三维数值模拟,采用有限体积法计算程式,求解不可压缩Navier-Stokes方程,模拟平板翼型在尾缘有无吹气时的流动情况,得到了平板翼型尾迹的传播特性。并使用四种常用湍流模型在相同的网格条件下进行数值模拟,模拟结果与相应的试验数据对比,分析各种湍流模型对带尾缘吹气的三维模型数值模拟结果的影响,得出了不同湍流模型对带尾缘吹气的模型的适用性以及精度的评估性结论。数值模拟的结果表明SST湍流模拟对模拟尾迹区流动具有很好的适应性,预测得到的轴向速度分布、尾迹特征长度变化以及流动相似性和试验结果进行了对比,和试验结果吻合较好。 A viscous,incompressible and 3D flow around a plate airfoil was numerically simulated using CFD software.The finite volume method for incompressible Navier-Stokes equations is employed in the program to simulate the flow in the wake of the plate airfoil with and without trailing edge blowing.The wake spreading characteristics of the airfoil are gained through the simulation.The CFD simulation was carried out using four turbulence models in the commercial CFD software under the same grid system.Then results were compared with the experimental results.The turbulence model effect to the wake flow simulation of plate airfoil with trailing edge blowing was analyzed and gains the evaluating conclusion of the turbulence model adaptability on the model with trailing edge blowing.According to the simulation results,SST turbulence model shows well adaptability to simulate the wake flow.The axial velocity profile,wake characteristic length scale and flow similarity gained through CFD simulation using SST turbulence model agree well with the experiment.
机构地区 上海交通大学
出处 《流体机械》 CSCD 北大核心 2011年第12期18-22,83,共6页 Fluid Machinery
关键词 尾迹 无动量亏损尾迹 数值模拟 湍流模型 尾缘吹气 wake momentumless wake numerical simulation turbulence model trailing edge blowing
  • 相关文献

参考文献8

  • 1Cimbala J M, Park W J. An experimental investigation of the turbulent structure in a two -dimensional momentumless wake [ J ]. Journal of Fluid Mechanics, 1990, (213) :479-509.
  • 2Jong Woo Ahn, Hyung Jin Sung, Prediction of two-di- mensional momentumless wake by k-e/model [ J ]. AIAA Journal,1995, 33(4) :611-617.
  • 3Cho J R, Chung M K. A proposal of k-a-yequation turbulence model [ J ]. Journal of Fluid Mechanics, 1992 (237) :301-322.
  • 4Cherepanov P Ya, Babenko V A, Experimental and numerical study of fiat momentumless wake [ J ]. International Journal of Heat and Fluid Flow, 1998, (19) :608-622.
  • 5林胜洋,竺晓程,沈昕,等.尾迹控制技术对叶栅性能的影响[A].2006中国工程热物理学会流体机械学术会议论文集[C].2006:102-107.
  • 6Sell Julian. Cascade testing to assess the effectiveness of mass addition/removal wake management strategies for reduction of rotor-stator interaction noise [ D ]. Master thesis, Massachusetts Institute of technology, 1997.
  • 7竺晓程,杜朝辉.带叶顶间隙轴流转子三维流动的数值模拟[J].上海交通大学学报,2003,37(9):1480-1483. 被引量:14
  • 8吴亚东,竺晓程,杜朝辉.无动量亏损尾迹的实验研究[J].实验流体力学,2007,21(3):30-34. 被引量:3

二级参考文献14

  • 1Van Zante D E, Hathaway M D, Wood J R, et al,Recommendations for achieving accurate numerical simulation of tip clearance flows in transonic compressor rotors[R]. Indiana: International Gas Turbine Aeroengine Congress & Exhibition, 1999.
  • 2Hah C. A numerical modeling of endwall and tipclearance flow of an isolated compressor rotor[J].Journal of Engineering for Gas Turbines and Power,1986,108:15--21.
  • 3Dawes W N. A numerical analysis of the three-dimensional viscous flow in a transonic compressor rotor and comparison with experiment[J]. Journal ot Turbomachinery, 1987, 109:83--90.
  • 4Basson A, Lakshminarayana B. Numerical simulation of tip clearance effects in turbomachinery[J]. Journal of Turbomachinery, 1995,117 : 348-- 359.
  • 5Inoue M, Kuroumaru M. Structure of tip clearance flow in an isolated axial compressor rotor [J]. Journal of Turbomachinery, 1989,111 : 250-- 256.
  • 6唐狄毅.叶轮机非定常流[M].北京:国防工业出版社,1992..
  • 7CIMBALA J M,PARK W J.An experimental investigation of the turbulent structure in a two-dimensional momentumless wake[J].Journal of Fluid Mechanics,1990,213:479-509.
  • 8PARK W J,CIMBALA J M.The effect of jet injection geometry on two dimensional momen--tumless wakes[J].Journal of Fluid Mechanics,1991,224:29-47.
  • 9LEITCH T A,SAUNDERS C A and NG W F.Reduction of unsteady stator rotor interaction using trailing edge blowing[J].Journal of Sound and Vibration,2000,232(2):235-245.
  • 10SELL J.Cascading testing to assess the effectiveness of mass addition/removal wake management strategies for reduction of rotor-stator interaction noise[D].MIT,Cambridge,MA,1997.

共引文献15

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部