Optimal control theory is combined with the numerical simulation of an incompressible viscous flow to control vortex shedding in order to maximize lift. A two-dimensional flat plate model is considered at a high angle of attack and a Reynolds number of 300. Actuation is provided by unsteady mass injection near the trailing edge and is modeled by a compact body force. The adjoint of the linearized perturbed equations is solved backwards in time to obtain the gradient of the lift to changes in actuation (the jet velocity), and this information is used to iteratively improve the controls. The optimized control waveform is nearly periodic and locked to vortex shedding. We investigate how features of the optimized waveform modify the vortex shed...
As opposed to conventional air vehicles that have fixed wings, small birds and insects are known to ...
As opposed to conventional air vehicles that have fixed wings, small birds and insects are known to ...
Active flow control is used to modify the lift, drag and pitching moments on a semicircular wing wit...
Optimal control theory is combined with the numerical simulation of an incompressible viscous flow t...
Optimal control theory is combined with the numerical simulation of an incompressible viscous flow t...
This thesis examines flow control and the potentially favorable effects of feedback, associated with...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high a...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high a...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high ...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high ...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high ...
The objective of this study is to employ feedback control to maximize time-average lift on a low-asp...
We study model-based feedback control of the low-Reynolds-number flow over a flat plate at large ang...
We study model-based feedback control of the low-Reynolds-number flow over a flat plate at large ang...
The objective of this study is to employ feedback control to maximize time-average lift on a low-asp...
As opposed to conventional air vehicles that have fixed wings, small birds and insects are known to ...
As opposed to conventional air vehicles that have fixed wings, small birds and insects are known to ...
Active flow control is used to modify the lift, drag and pitching moments on a semicircular wing wit...
Optimal control theory is combined with the numerical simulation of an incompressible viscous flow t...
Optimal control theory is combined with the numerical simulation of an incompressible viscous flow t...
This thesis examines flow control and the potentially favorable effects of feedback, associated with...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high a...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high a...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high ...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high ...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high ...
The objective of this study is to employ feedback control to maximize time-average lift on a low-asp...
We study model-based feedback control of the low-Reynolds-number flow over a flat plate at large ang...
We study model-based feedback control of the low-Reynolds-number flow over a flat plate at large ang...
The objective of this study is to employ feedback control to maximize time-average lift on a low-asp...
As opposed to conventional air vehicles that have fixed wings, small birds and insects are known to ...
As opposed to conventional air vehicles that have fixed wings, small birds and insects are known to ...
Active flow control is used to modify the lift, drag and pitching moments on a semicircular wing wit...