Distributed forcing of flow over a circular cylinder

被引:169
作者
Kim, J
Choi, H [1 ]
机构
[1] Seoul Natl Univ, Sch Mech & Aerosp Engn, Inst Adv Machinery & Design, Seoul 151744, South Korea
[2] Seoul Natl Univ, Ctr Turbulence & Flow Control Res, Inst Adv Machinery & Design, Seoul 151744, South Korea
关键词
D O I
10.1063/1.1850151
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In the present study, we apply a distributed (i.e., spatially varying) forcing to flow over a circular cylinder for drag reduction. The distributed forcing is realized by a blowing and suction from the slots located at upper and lower surfaces of the cylinder. The forcing profile from each slot is sinusoidal in the spanwise direction but is steady in time. We consider two different phase differences between the upper and lower blowing/suction profiles: zero (in-phase forcing) and pi (out-of-phase forcing). The Reynolds numbers considered are from 40 to 3900 covering various regimes of flow over a circular cylinder. For all the Reynolds numbers larger than 47, the present in-phase distributed forcing attenuates or annihilates the Karman vortex shedding and thus significantly reduces the mean drag and the drag and lift fluctuations. The optimal wavelength and amplitude of the in-phase forcing for maximum drag reduction are also obtained for the Reynolds number of 100. It is shown that the in-phase forcing produces the phase mismatch along the spanwise direction in the vortex shedding, weakens the strength of vortical structures in the wake, and thus reduces the drag. Unlike the in-phase forcing, the out-of-phase distributed forcing does not reduce the drag at low Reynolds numbers, but it reduces the mean drag and the drag and lift fluctuations at a high Reynolds number of 3900 by affecting the evolution of the separating shear layer, although the amount of drag reduction is smaller than that by the in-phase forcing. (C) 2005 American Institute of Physics.
引用
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页码:033103 / 1
页数:16
相关论文
共 45 条
[1]   TRANSVERSE FLOW OVER A WAVY CYLINDER [J].
AHMED, A ;
BAYSMUCHMORE, B .
PHYSICS OF FLUIDS A-FLUID DYNAMICS, 1992, 4 (09) :1959-1967
[2]   Role of actuation frequency in controlled flow reattachment over a stalled airfoil [J].
Amitay, M ;
Glezer, A .
AIAA JOURNAL, 2002, 40 (02) :209-216
[4]   EFFECT OF BASE BLEED ON FLOW BEHIND A 2-DIMENSIONAL MODEL WITH A BLUNT TRAILING EDGE [J].
BEARMAN, PW .
AERONAUTICAL QUARTERLY, 1967, 18 :207-&
[5]   Reduction of bluff-body drag and suppression of vortex shedding by the introduction of wavy separation lines [J].
Bearman, PW ;
Owen, JC .
JOURNAL OF FLUIDS AND STRUCTURES, 1998, 12 (01) :123-130
[6]   EFFECTS OF IMPOSED SPANWISE PERTURBATIONS ON PLANE MIXING-LAYER STRUCTURE [J].
BELL, JH ;
MEHTA, RD .
JOURNAL OF FLUID MECHANICS, 1993, 257 :33-63
[7]  
Choi H., 1992, Report No. TF-55
[8]   Effect of spanwise-varying local forcing on turbulent separated flow over a backward-facing step [J].
Chun, S ;
Lee, I ;
Sung, HJ .
EXPERIMENTS IN FLUIDS, 1999, 26 (05) :437-440
[9]   THE EVOLUTION OF A PLANE MIXING LAYER WITH SPANWISE NONUNIFORM FORCING [J].
COLLIS, SS ;
LELE, SK ;
MOSER, RD ;
ROGERS, MM .
PHYSICS OF FLUIDS, 1994, 6 (01) :381-396
[10]   The suppression of lift on a circular cylinder due to vortex shredding at moderate Reynolds numbers [J].
Dalton, C ;
Xu, Y ;
Owen, JC .
JOURNAL OF FLUIDS AND STRUCTURES, 2001, 15 (3-4) :617-628