International audienceIn this Brief Communication we are interested in the maximum mean drag reduction that can be achieved under rotary sinusoidal control for the circular cylinder wake in the laminar regime. For a Reynolds number equal to 200, we give numerical evidence that partial control restricted to an upstream part of the cylinder surface may considerably increase the effectiveness of the control. Indeed, a maximum value of relative mean drag reduction equal to 30% is obtained when applying a specific sinusoidal control to the whole cylinder, where up to 75% of reduction can be obtained when the same control law is applied only to a well-selected upstream part of the cylinder. This result suggests that a mean flow correction field w...
It has been observed by researchers in the past that vortex shedding behind circular cylinders can b...
In this paper, the wake control of a circular cylinder by dual plates symmetrically attached at the ...
Boundary layer separation is the principal cause for the relatively large drag force experienced by ...
International audienceIn this Brief Communication we are interested in the maximum mean drag reducti...
International audienceIn this Brief Communication, we determine an approximate relation that gives t...
International audienceWe report high drag reduction in Direct Numerical Simulations of controled flo...
The classical problem of suppressing vortex shedding in the wake of a circular cylinder by using bod...
International audienceIn this paper we investigate the optimal control approach for the active contr...
This study is focused on two- and three-dimensional incompressible flow past a circular cylinder for...
International audienceThis study assesses the ability of a sensitivity-based, span-wise homogeneous ...
International audienceIn this paper we investigate the optimal control approach for the active contr...
Drag reduction in two-dimensional flow over a circular cylinder, achieved using rotary oscillation, ...
Exploratory experiments have been performed on circular cylinders executing forced rotary oscillatio...
The control of bluff-body wakes for reduced drag and enhanced stability has traditionally relied on ...
The effects of installing a small control rod upstream of a circular cylinder are investigated exper...
It has been observed by researchers in the past that vortex shedding behind circular cylinders can b...
In this paper, the wake control of a circular cylinder by dual plates symmetrically attached at the ...
Boundary layer separation is the principal cause for the relatively large drag force experienced by ...
International audienceIn this Brief Communication we are interested in the maximum mean drag reducti...
International audienceIn this Brief Communication, we determine an approximate relation that gives t...
International audienceWe report high drag reduction in Direct Numerical Simulations of controled flo...
The classical problem of suppressing vortex shedding in the wake of a circular cylinder by using bod...
International audienceIn this paper we investigate the optimal control approach for the active contr...
This study is focused on two- and three-dimensional incompressible flow past a circular cylinder for...
International audienceThis study assesses the ability of a sensitivity-based, span-wise homogeneous ...
International audienceIn this paper we investigate the optimal control approach for the active contr...
Drag reduction in two-dimensional flow over a circular cylinder, achieved using rotary oscillation, ...
Exploratory experiments have been performed on circular cylinders executing forced rotary oscillatio...
The control of bluff-body wakes for reduced drag and enhanced stability has traditionally relied on ...
The effects of installing a small control rod upstream of a circular cylinder are investigated exper...
It has been observed by researchers in the past that vortex shedding behind circular cylinders can b...
In this paper, the wake control of a circular cylinder by dual plates symmetrically attached at the ...
Boundary layer separation is the principal cause for the relatively large drag force experienced by ...