Experimental assessment of square-wave spatial spanwise forcing of a turbulent boundary layer

被引:4
作者
Knoop, Max W. [1 ]
Hartog, Friso H. [1 ,2 ]
Schrijer, Ferdinand F. J. [1 ]
van Campenhout, Olaf W. G. [1 ,2 ]
van Nesselrooij, Michiel [1 ,2 ]
van Oudheusden, Bas W. [1 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, Kluyverweg 1, NL-2629 HS Delft, Netherlands
[2] Dimple Aerosp BV, Kluyverweg 1, NL-2629 HS Delft, Netherlands
关键词
DRAG-REDUCTION; MOTION; FLOW;
D O I
10.1007/s00348-024-03799-9
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
We present an experimental realisation of spatial spanwise forcing in a turbulent boundary layer flow, aimed at reducing the frictional drag. The forcing is achieved by a series of spanwise running belts, running in alternating spanwise direction, thereby generating a steady spatial square-wave forcing. Stereoscopic particle image velocimetry in the streamwise-wall-normal plane is used to investigate the impact of actuation on the flow in terms of turbulence statistics, drag performance characteristics, and spanwise velocity profiles, for a non-dimensional wavelength of lambda(+)(x) = 397. In line with reported numerical studies, we confirm that a significant flow control effect can be realised with this type of forcing. The scalar fields of the higher-order turbulence statistics show a strong attenuation of stresses and production of turbulence kinetic energy over the first belt already, followed by a more gradual decrease to a steady-state energy response over the second belt. The stream-wise velocity in the near-wall region is reduced, indicative of a drag-reduced flow state. The profiles of the higher-order turbulence statistics are attenuated up to a wall-normal height of y(+) approximate to 100, with a maximum streamwise stress reduction of 45% and a reduction of integral turbulence kinetic energy production of 39%, for a non-dimensional actuation amplitude of A(+) = 12.7. An extension of the classical laminar Stokes layer theory is introduced, based on the linear superposition of Fourier modes, to describe the non-sinusoidal boundary condition that corresponds to the current case. The experimentally obtained spanwise velocity profiles show good agreement with this extended theoretical model. The drag reduction was estimated from a linear fit in the viscous sublayer in the range 2 <= y(+) <= 5. The results are found to be in good qualitative agreement with the numerical implementations of Viotti et al. ( Phys Fluids 21, 2009), matching the drag reduction trend with A(+), and reaching a maximum of 20%.
引用
收藏
页数:16
相关论文
共 32 条
[1]   Spanwise oscillatory wall motion in channel flow: drag-reduction mechanisms inferred from DNS-predicted phase-wise property variations at Reτ=1000 [J].
Agostini, L. ;
Touber, E. ;
Leschziner, M. A. .
JOURNAL OF FLUID MECHANICS, 2014, 743 :606-635
[2]   Experimental assessment of drag reduction by traveling waves in a turbulent pipe flow [J].
Auteri, F. ;
Baron, A. ;
Belan, M. ;
Campanardi, G. ;
Quadrio, M. .
PHYSICS OF FLUIDS, 2010, 22 (11)
[3]   Wall-drag measurements of smooth- and rough-wall turbulent boundary layers using a floating element [J].
Baars, W. J. ;
Squire, D. T. ;
Talluru, K. M. ;
Abbassi, M. R. ;
Hutchins, N. ;
Marusic, I. .
EXPERIMENTS IN FLUIDS, 2016, 57 (05)
[4]  
Baron A, 1995, APPL SCI RES, V55, P311, DOI 10.1007/BF00856638
[5]   Experimental Control of Turbulent Boundary Layers with In-plane Travelling Waves [J].
Bird, James ;
Santer, Matthew ;
Morrison, Jonathan F. .
FLOW TURBULENCE AND COMBUSTION, 2018, 100 (04) :1015-1035
[6]   MEASUREMENTS IN THE TURBULENT BOUNDARY-LAYER ON AN INFINITE SWEPT WING [J].
BRADSHAW, P ;
PONTIKOS, NS .
JOURNAL OF FLUID MECHANICS, 1985, 159 (OCT) :105-130
[7]   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)
[8]   Drag reduction by spanwise wall oscillation in wall-bounded turbulent flows [J].
Choi, JI ;
Xu, CX ;
Sung, HJ .
AIAA JOURNAL, 2002, 40 (05) :842-850
[9]   Near-wall structure of turbulent boundary layer with spanwise-wall oscillation [J].
Choi, KS .
PHYSICS OF FLUIDS, 2002, 14 (07) :2530-2542
[10]   Prediction of turbulence control for arbitrary periodic spanwise wall movement [J].
Cimarelli, Andrea ;
Frohnapfel, Bettina ;
Hasegawa, Yosuke ;
De Angelis, Elisabetta ;
Quadrio, Maurizio .
PHYSICS OF FLUIDS, 2013, 25 (07)