Comparison of DDES and URANS for Unsteady Tip Leakage Flow in an Axial Compressor Rotor

被引:59
|
作者
Liu, Yangwei [1 ,2 ]
Zhong, Luyang [1 ]
Lu, Lipeng [1 ,2 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China
[2] Beihang Univ, Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
LARGE-EDDY SIMULATION; CORNER SEPARATION; TURBULENCE MODELS; CLEARANCE FLOW; VORTEX;
D O I
10.1115/1.4043774
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Tip leakage vortex (TLV) has a large impact on compressor performance and should be accurately predicted by computational fluid dynamics (CFD) methods. New approaches of turbulence modeling, such as delayed detached eddy simulation (DDES), have been proposed, the computational resources of which can be reduced much more than for large eddy simulation (LES). In this paper, the numerical simulations of the rotor in a low-speed large-scale axial compressor based on DDES and unsteady Reynoldsaveraged Navier-Stokes (URANS) are performed, thus improving our understanding of the TLV dynamic mechanisms and discrepancy of these two methods. We compared the influence of different time steps in the URANS simulation. The widely used large timestep makes the unsteadiness extremely weak. The small time-step shows a better result close to DDES. The time-step scale is related to the URANS unsteadiness and should be carefully selected. In the time-averaged flow, the TLV in DDES dissipates faster, which has a more similar structure to the experiment. Then, the time-averaged and instantaneous results are compared to divide the TLV into three parts. URANS cannot give the loss of stability and evolution details of TLV. The fluctuation velocity spectra show that the amplitude of high frequencies becomes obvious downstream from the TLV, where it becomes unstable. Last, the anisotropy of the Reynolds stress of these two methods is analyzed through the Lumley triangle to see the distinction between the methods and obtain the Reynolds stress. The results indicate that the TLV latter part in DDES is anisotropic, while in URANS it is isotropic.
引用
收藏
页数:13
相关论文
共 50 条
  • [1] COMPARISON OF DDES AND URANS FOR UNSTEADY TIP LEAKAGE FLOW IN AN AXIAL COMPRESSOR ROTOR
    Liu, Yangwei
    Zhong, Luyang
    Lu, Lipeng
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 2A, 2018,
  • [2] Behavior of tip leakage flow in an axial flow compressor rotor
    Wu, Yanhui
    Chu, Wuli
    Lu, Xingen
    Zhu, Junqiang
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 6, PTS A AND B, 2006, : 195 - 204
  • [3] Unsteady Tip Clearance Flow in an Isolated Axial Compressor Rotor
    H ongwu ZHANG1 Xiangyang DENG1
    [J]. Journal of Thermal Science, 2005, (03) : 21 - 29
  • [4] Unsteady tip clearance flow in an isolated axial compressor rotor
    Hongwu Zhang
    Xiangyang Deng
    Jingyi Chen
    Weiguang Huang
    [J]. Journal of Thermal Science, 2005, 14 : 211 - 219
  • [5] Unsteady Tip Clearance Flow in an Isolated Axial Compressor Rotor
    Zhang, Hongwu
    Deng, Xiangyang
    Chen, Jingyi
    Huang, Weiguang
    [J]. JOURNAL OF THERMAL SCIENCE, 2005, 14 (03) : 211 - 219
  • [6] BEHAVIOR OF TIP LEAKAGE FLOW BEHIND AN AXIAL COMPRESSOR ROTOR
    INOUE, M
    KUROUMARU, M
    FUKUHARA, M
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1986, 108 (01): : 7 - 14
  • [7] Behaviour of tip-leakage flow in an axial flow compressor rotor
    Wu, Y.
    Chu, W.
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2007, 221 (A1) : 99 - 110
  • [8] NUMERICAL STUDY ON TIP LEAKAGE FLOW STRUCTURE OF AN AXIAL FLOW COMPRESSOR ROTOR
    Zhang, Chenkai
    Hu, Jun
    Wang, Zhiqiang
    Yan, Wei
    Yin, Chao
    Gao, Xiang
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 2A, 2014,
  • [9] Quantitative evaluation of the unsteady behaviors of the tip leakage vortex in a subsonic axial compressor rotor
    Liu, Baojie
    An, Guangfeng
    Yu, Xianjun
    Zhang, Zhibo
    [J]. EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2016, 79 : 154 - 167
  • [10] Experimental investigation of flow characteristic of tip leakage flow in an axial flow compressor rotor
    Wu, Yanhui
    An, Guangyao
    Wu, Junfeng
    Jia, Yizhe
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2015, 229 (02) : 112 - 126