The potential benefits of active flow control are no more debated. Among many others applications, flow control provides an effective mean for manipulating turbulent separated flows. Here, a nonthermal surface plasma discharge (dielectric barrier discharge) is installed at the step corner of a backward-facing step (U 0 = 15 m/s, Re h = 30,000, Re θ = 1650). Wall pressure sensors are used to estimate the reattaching location downstream of the step (objective function #1) and also to measure the wall pressure fluctuation coefficients (objective function #2). An autonomous multi-variable optimization by genetic algorithm is implemented in an experiment for optimizing...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma a...
Turbulent flow has a significantly higher drag than the corresponding laminar flow at the same flow ...
The continued high global demand for passenger and freight air traffic along with increased use of u...
The final publication is available at Springer via http://dx.doi.org/10.1007/s00348-015-2107-3The po...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revolution...
The practical interest of flow control approaches is no more debated as flow control provides an eff...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revol...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasm...
In this paper, the application of the surface mass transfer optimization in shock wave-boundary laye...
Due to the more stringent aviation regulations on fuel consumption and noise reduction, the interest...
The convective heat transfer in a turbulent boundary layer (TBL) on a flat plate is enhanced using a...
Active flow control is an area of heightened interest in the aerospace community. Previous research ...
We experimentally perform open and closed-loop control of a separating turbulent boundary layer down...
This thesis addresses the problem of controlling the unsteady flow separation over an aerofoil using...
Plasma actuators are devices which function by creating a discharge in air at atmospheric conditions...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma a...
Turbulent flow has a significantly higher drag than the corresponding laminar flow at the same flow ...
The continued high global demand for passenger and freight air traffic along with increased use of u...
The final publication is available at Springer via http://dx.doi.org/10.1007/s00348-015-2107-3The po...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revolution...
The practical interest of flow control approaches is no more debated as flow control provides an eff...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revol...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasm...
In this paper, the application of the surface mass transfer optimization in shock wave-boundary laye...
Due to the more stringent aviation regulations on fuel consumption and noise reduction, the interest...
The convective heat transfer in a turbulent boundary layer (TBL) on a flat plate is enhanced using a...
Active flow control is an area of heightened interest in the aerospace community. Previous research ...
We experimentally perform open and closed-loop control of a separating turbulent boundary layer down...
This thesis addresses the problem of controlling the unsteady flow separation over an aerofoil using...
Plasma actuators are devices which function by creating a discharge in air at atmospheric conditions...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma a...
Turbulent flow has a significantly higher drag than the corresponding laminar flow at the same flow ...
The continued high global demand for passenger and freight air traffic along with increased use of u...