Direct numerical simulation of the flow around a wall-mounted square cylinder under various inflow conditions

被引:63
作者
Vinuesa, Ricardo [1 ]
Schlatter, Philipp [1 ]
Malm, Johan [1 ]
Mavriplis, Catherine [2 ]
Henningson, Dan S. [1 ]
机构
[1] KTH Mech, Linne FLOW Ctr, Stockholm, Sweden
[2] Univ Ottawa, Dept Mech Engn, Ottawa, ON K1N 6N5, Canada
基金
加拿大自然科学与工程研究理事会; 瑞典研究理事会;
关键词
wall turbulence; direct numerical simulation; three-dimensional flows; separated flows; square-cylinder flow; TURBULENCE MODELS; BOUNDARY-LAYERS; ASPECT RATIO; WAKE; LENGTH; NUMBERS;
D O I
10.1080/14685248.2014.989232
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The flow around a wall-mounted square cylinder of side d is investigated by means of direct numerical simulation (DNS). The effect of inflow conditions is assessed by considering two different cases with matching momentum-thickness Reynolds numbers Re-theta similar or equal to 1000 at the obstacle: the first case is a fullyturbulent zero pressure gradient boundary layer, and the second one is a laminar boundary layer with prescribed Blasius inflow profile further upstream. An auxiliary simulation carried out with the pseudo-spectral Fourier-Chebyshev code SIMSON is used to obtain the turbulent time-dependent inflow conditions which are then fed into the main simulation where the actual flow around the cylinder is computed. This main simulation is performed, for both laminar and turbulent-inflows, with the spectral-element method code Nek5000. In both cases the wake is completely turbulent, and we find the same Strouhal number St similar or equal to 0.1, although the two wakes exhibit structural differences for x > 3d downstream of the cylinder. Transition to turbulence is observed in the laminar-inflow case, induced by the recirculation bubble produced upstream of the obstacle, and in the turbulent-inflow simulation the streamwise fluctuations modulate the horseshoe vortex. The wake obtained in our laminar-inflow case is in closer agreement with reference particle image velocimetry measurements of the same geometry, revealing that the experimental boundary layer was not fully turbulent in that dataset, and highlighting the usefulness of DNS to assess the quality of experimental inflow conditions.
引用
收藏
页码:555 / 587
页数:33
相关论文
共 49 条
[1]   Coherent vortical and straining structures in the finite wall-mounted square cylinder wake [J].
Bourgeois, J. A. ;
Sattari, P. ;
Martinuzzi, R. J. .
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2012, 35 :130-140
[2]   Criteria for assessing experiments in zero pressure gradient boundary layers [J].
Chauhan, Kapil A. ;
Monkewitz, Peter A. ;
Nagib, Hassan M. .
FLUID DYNAMICS RESEARCH, 2009, 41 (02)
[3]  
Chen Z., 2012, P 20 ANN C CFD SOC C
[4]   Modeling artificial boundary conditions for compressible flow [J].
Colonius, T .
ANNUAL REVIEW OF FLUID MECHANICS, 2004, 36 :315-345
[5]   FLOW NEAR A BUILDING MODEL IN A FAMILY OF SURFACE-LAYERS [J].
CORKE, TC ;
NAGIB, HM ;
TANATICHAT, J .
JOURNAL OF INDUSTRIAL AERODYNAMICS, 1979, 5 (1-2) :139-158
[6]  
Fischer P F., 2008, nek5000 Web page
[7]   VORTICAL STRUCTURE IN THE WAKE OF A TRANSVERSE JET [J].
FRIC, TF ;
ROSHKO, A .
JOURNAL OF FLUID MECHANICS, 1994, 279 :1-47
[8]   Pressure gradient effects on the large-scale structure of turbulent boundary layer [J].
Harun, Zambri ;
Monty, Jason P. ;
Mathis, Romain ;
Marusic, Ivan .
JOURNAL OF FLUID MECHANICS, 2013, 715 :477-498
[9]   Simulations of turbulent flow in a plane asymmetric diffuser [J].
Herbst, A. H. ;
Schlatter, P. ;
Henningson, D. S. .
FLOW TURBULENCE AND COMBUSTION, 2007, 79 (03) :275-306
[10]   Energy balance for turbulent flow around a surface mounted cube placed in a channel [J].
Hussein, HJ ;
Martinuzzi, RJ .
PHYSICS OF FLUIDS, 1996, 8 (03) :764-780