INVESTIGATION OF TURBULENCE CHARACTERISTICS IN A TIP LEAKAGE FLOW MODEL USING LARGE-EDDY SIMULATION

被引:0
作者
Gao, Yanfei [1 ]
Liu, Yangwei [1 ,2 ]
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
来源
PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 2A | 2019年
基金
中国国家自然科学基金;
关键词
CORNER SEPARATION; STALL INCEPTION; VORTEX; MECHANISMS; CLEARANCE;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A simple tip leakage flow (TLF) model which consists of a square duct with a longitudinal slit on the top of a side wall is proposed to reproduce the jet flow/main flow shear mechanism of the tip leakage vortex (TLV) rolling-up in turbomachinery. Large-eddy simulation (LES) is employed to investigate the turbulence characteristics of the flow model under low Reynolds number condition. The geometry and boundary conditions of the flow model are simplified from a compressor rotor and modified to apply to low-Re condition for LES. The vortex structures and turbulence characteristics of the LES results are compared with the measurements of the rotor. It is found that the flow model could reproduce similar flow field and turbulence structures compared with the TLF in the real rotor, thus it can be used to investigate the turbulence in practical flows. Reynolds-Averaged Navier-Stokes (RANS) calculations are also carried out. The mean flow and turbulence behaviors of different cases are analyzed. The budgets of turbulent kinetic energy (k) are analyzed to investigate the turbulence transport nature in the TLF model, indicating that the non-equilibrium transport process of k is significant, especially the pressure and turbulent transport, which is not predicted by RANS.
引用
收藏
页数:13
相关论文
共 35 条
[1]   THE ROLE OF TIP CLEARANCE IN HIGH-SPEED FAN STALL [J].
ADAMCZYK, JJ ;
CELESTINA, ML ;
GREITZER, EM .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1993, 115 (01) :28-39
[2]  
[Anonymous], 2014, THESIS
[3]   ROTOR-TIP LEAKAGE .1. BASIC METHODOLOGY [J].
BOOTH, TC ;
DODGE, PR ;
HEPWORTH, HK .
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1982, 104 (01) :154-161
[4]   Assessment Measures for Engineering LES Applications [J].
Celik, I. ;
Klein, M. ;
Janicka, J. .
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2009, 131 (03) :0311021-03110210
[5]   RANS and LES computations of the tip-leakage vortex for different gap widths [J].
Decaix, J. ;
Balarac, G. ;
Dreyer, M. ;
Farhat, M. ;
Muench, C. .
JOURNAL OF TURBULENCE, 2015, 16 (04) :309-341
[6]   THE 1993 IGTI SCHOLAR LECTURE - LOSS MECHANISMS IN TURBOMACHINES [J].
DENTON, JD .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1993, 115 (04) :621-656
[7]  
Denton JD, 2010, PROCEEDINGS OF THE ASME TURBO EXPO 2010: TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS DESIGN METHODS, AND CFD MODELING FOR TURBOMACHINERY, VOL 7, PTS A-C, P735
[8]   Relationship between the Flow Blockage of Tip Leakage Vortex and its Evolutionary Procedures inside the Rotor Passage of a Subsonic Axial Compressor [J].
Du Hui ;
Yu Xianjun ;
Zhang Zhibo ;
Liu Baojie .
JOURNAL OF THERMAL SCIENCE, 2013, 22 (06) :522-531
[9]   The role of tip leakage vortex breakdown in compressor rotor aerodynamics [J].
Furukawa, M ;
Inoue, M ;
Saiki, K ;
Yamada, K .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1999, 121 (03) :469-480
[10]   Study of the Standard k-ε Model for Tip Leakage Flow in an Axial Compressor Rotor [J].
Gao, Yanfei ;
Liu, Yangwei ;
Zhong, Luyang ;
Hou, Jiexuan ;
Lu, Lipeng .
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 33 (04) :353-360