Since 1947, when Schubauer and Skramstad established the basis of the technology with its revolutionary work about steady state tools and mechanisms for the flow management, the progress of the flow control technology and the development of devices have progressed constantly. Anyway, the applicability of such devices is limited, and only few of them have arrived to the assembly workshop. The problem is that the range of actuation is still limited. Despite their operability limitations, flow control devices are of great interest for the aeronautical industry. The number of projects investigating this technology demonstrates the relevance of in the Fluid Dynamic field. The scientific interest focus not only on the industrial applications and ...
Active control of the flow over an airfoil is an area of heightened interest in the aerospace commun...
This study investigates the application of two advanced optimization methods for solving active flow...
The high-level objective of MARS project was to understand the formation and behaviour of turbulent ...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revolution...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revol...
The potential benefits of active flow control are no more debated. Among many others applications, f...
The practical interest of flow control approaches is no more debated as flow control provides an eff...
The goal of this thesis was to both theoretically and experimentally show the effect of a plasma act...
Active flow control is an area of heightened interest in the aerospace community. Previous research ...
The paper investigates two advanced optimisation methods for solving active flow control device shap...
The use of Active Flow Control (AFC) technologies to modify the forces acting on streamlined bodies ...
Turbulent flow separation over a wall-mounted hump model and its control using plasma actuators were...
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...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma a...
Active control of the flow over an airfoil is an area of heightened interest in the aerospace commun...
This study investigates the application of two advanced optimization methods for solving active flow...
The high-level objective of MARS project was to understand the formation and behaviour of turbulent ...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revolution...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revol...
The potential benefits of active flow control are no more debated. Among many others applications, f...
The practical interest of flow control approaches is no more debated as flow control provides an eff...
The goal of this thesis was to both theoretically and experimentally show the effect of a plasma act...
Active flow control is an area of heightened interest in the aerospace community. Previous research ...
The paper investigates two advanced optimisation methods for solving active flow control device shap...
The use of Active Flow Control (AFC) technologies to modify the forces acting on streamlined bodies ...
Turbulent flow separation over a wall-mounted hump model and its control using plasma actuators were...
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...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma a...
Active control of the flow over an airfoil is an area of heightened interest in the aerospace commun...
This study investigates the application of two advanced optimization methods for solving active flow...
The high-level objective of MARS project was to understand the formation and behaviour of turbulent ...