TY - JOUR
T1 - Effect of uniform blowing/suction in a turbulent boundary layer at moderate Reynolds number
AU - Kametani, Yukinori
AU - Fukagata, Koji
AU - Örlü, Ramis
AU - Schlatter, Philipp
N1 - Funding Information:
This work was partly supported through Grant-in-Aid for Scientific Research (C) (No. 25420129 ) and Grant-in-Aid for JSPS Fellows (No. 24-3450 ) by Japan Society for the Promotion of Science (JSPS). Financial support by the Knut and Alice Wallenberg Foundation is also gratefully acknowledged. Computer time is provided by Swedish National Infrastructure for Computing (SNIC).
PY - 2015/10/1
Y1 - 2015/10/1
N2 - A number of well-resolved large-eddy simulations (LES) of a spatially evolving turbulent boundary layer with uniform blowing or suction is performed in order to investigate the effect on skin friction drag as well as turbulence statistics and spectral composition at moderate Reynolds numbers up to Reθ=2500, based on the free-stream velocity and the momentum-loss thickness. The amplitude of uniform blowing or suction is set to be 0.1% of the free-stream velocity with different streamwise ranges of the controlled region.The boundary layer is thickened by blowing and thinned by suction. The Reynolds shear and normal stresses are increased by blowing and decreased by suction, most prominently, in the outer region. Through spectral analysis of the streamwise velocity and cross-spectra of the Reynolds shear stress, the enhancement and reduction of the fluctuation energy in the outer region by blowing and suction are found, respectively. It is also found that the emergence of a second peak in the outer region is promoted by blowing, while it is inhibited in the case of suction.In spite of the weak amplitude of the control, more than 10% of drag reduction and enhancement are achieved by means of blowing and suction, respectively. In the case of blowing, where drag reduction is achieved, the mean drag reduction rate increases as the blowing region extends because the local reduction rate, i.e.the streamwise gradient of the mean drag reduction rate, grows in the streamwise direction. The net-energy saving rate and the control gain have the same trends. It is found that a more effective skin friction drag reduction and control efficiency can be achieved with a wider control region that starts at a more upstream location.
AB - A number of well-resolved large-eddy simulations (LES) of a spatially evolving turbulent boundary layer with uniform blowing or suction is performed in order to investigate the effect on skin friction drag as well as turbulence statistics and spectral composition at moderate Reynolds numbers up to Reθ=2500, based on the free-stream velocity and the momentum-loss thickness. The amplitude of uniform blowing or suction is set to be 0.1% of the free-stream velocity with different streamwise ranges of the controlled region.The boundary layer is thickened by blowing and thinned by suction. The Reynolds shear and normal stresses are increased by blowing and decreased by suction, most prominently, in the outer region. Through spectral analysis of the streamwise velocity and cross-spectra of the Reynolds shear stress, the enhancement and reduction of the fluctuation energy in the outer region by blowing and suction are found, respectively. It is also found that the emergence of a second peak in the outer region is promoted by blowing, while it is inhibited in the case of suction.In spite of the weak amplitude of the control, more than 10% of drag reduction and enhancement are achieved by means of blowing and suction, respectively. In the case of blowing, where drag reduction is achieved, the mean drag reduction rate increases as the blowing region extends because the local reduction rate, i.e.the streamwise gradient of the mean drag reduction rate, grows in the streamwise direction. The net-energy saving rate and the control gain have the same trends. It is found that a more effective skin friction drag reduction and control efficiency can be achieved with a wider control region that starts at a more upstream location.
KW - Drag reduction
KW - Large-eddy simulation
KW - Turbulent boundary layer
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U2 - 10.1016/j.ijheatfluidflow.2015.05.019
DO - 10.1016/j.ijheatfluidflow.2015.05.019
M3 - Article
AN - SCOPUS:84945456169
SN - 0142-727X
VL - 55
SP - 132
EP - 142
JO - Heat Fluid Flow
JF - Heat Fluid Flow
ER -