Turbulent flow and noise sources on a circular cylinder in the critical regime

被引:17
作者
Zhang, Chaofan [1 ]
Moreau, Stephane [1 ]
Sanjose, Marlene [1 ]
机构
[1] Univ Sherbrooke, Dept Mech Engn, 2500 Blvd Univ, Sherbrooke, PQ J1K 2R1, Canada
关键词
EXCITED ACOUSTIC-RESONANCE; PARTICLE IMAGE VELOCIMETRY; LARGE-EDDY SIMULATION; CROSS-FLOW; NUMERICAL-SIMULATION; SKIN-FRICTION; WAKE; TRANSITION; GENERATION; SMOOTH;
D O I
10.1063/1.5121544
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The flow around a circular cylinder with long spanwise length has been investigated in the critical regime using a compressible wall-resolved Large Eddy Simulation (LES) for the first time. The flow at such a critical Reynolds number combines complex features: large favorable and adverse pressure gradient, separation and turbulence transition and flow reattachment. The results of the present simulation agree well with previous experimental and incompressible LES data, for the distribution of the mean wall-pressure coefficient that dominates the drag coefficient, and the skin-friction coefficient that illustrates the flow separation and reattachment behaviors. A weak reattachment is observed from the quasi-zero skin-friction in the reattachment region. A detailed study of the boundary-layer and shear-layer development around the cylinder with profiles of mean velocity and turbulence intensities confirms the transition, separation and reattachment behaviors shown by the skin-friction coefficient. The maximum tangential velocity and its location above the wall have also proven to be adequate measures of the edge velocity and associated boundary layer thickness. The Kelvin-Helmholtz instabilities have been observed in the shear layer and the ratio of the frequency of these instabilities and the fundamental vortex shedding frequency matches well with the existing scaling based on experimental data. The far-field noise obtained by both direct computation and acoustic analogy shows a dominant vortex shedding tone, but with additional broadband sources in the cylinder wake. These sound sources are evaluated from maps of filtered pressure signals and cross-correlation analysis of the pressure fluctuations around the cylinder and in the far-field. (C) 2019 Author(s).
引用
收藏
页数:16
相关论文
共 61 条
[2]   ON VORTEX SHEDDING FROM SMOOTH AND ROUGH CYLINDERS IN THE RANGE OF REYNOLDS-NUMBERS 6X103 TO 5X106 [J].
ACHENBACH, E ;
HEINECKE, E .
JOURNAL OF FLUID MECHANICS, 1981, 109 (AUG) :239-251
[3]   TOTAL AND LOCAL HEAT-TRANSFER FROM A SMOOTH CIRCULAR-CYLINDER IN CROSS-FLOW AT HIGH REYNOLDS-NUMBER [J].
ACHENBACH, E .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1975, 18 (12) :1387-1396
[4]   INFLUENCE OF SURFACE ROUGHNESS ON CROSS-FLOW AROUND A CIRCULAR CYLINDER [J].
ACHENBACH, E .
JOURNAL OF FLUID MECHANICS, 1971, 46 (MAR29) :321-+
[5]  
[Anonymous], THESIS
[6]   ON VORTEX SHEDDING FROM A CIRCULAR CYLINDER IN CRITICAL REYNOLDS NUMBER REGIME [J].
BEARMAN, PW .
JOURNAL OF FLUID MECHANICS, 1969, 37 :577-&
[7]  
Beaudan P., 1994, TF62 STANF U
[8]   THE TRANSITION TO TURBULENCE IN THE WAKE OF A CIRCULAR CYLINDER [J].
BLOOR, MS .
JOURNAL OF FLUID MECHANICS, 1964, 19 (02) :290-&
[9]   Lattice-Boltzmann Aeroacoustic Analysis of the LAGOON Landing-Gear Configuration [J].
Casalino, Damiano ;
Ribeiro, Andre F. P. ;
Fares, Ehab ;
Noelting, Swen .
AIAA JOURNAL, 2014, 52 (06) :1232-1248
[10]   Large-eddy simulation of flow over a cylinder with ReD from 3.9 x 103 to 8.5 x 105: a skin-friction perspective [J].
Cheng, W. ;
Pullin, D. I. ;
Samtaney, R. ;
Zhang, W. ;
Gao, W. .
JOURNAL OF FLUID MECHANICS, 2017, 820 :121-158