University of Minnesota M.S.E.E. thesis. August 2018. Major: Electrical/Computer Engineering. Advisor: Maziar Hemati. 1 computer file (PDF); vii, 60 pages.Flow separation leads to degraded performance in many engineering systems. Several flow control strategies have been developed to mitigate flow separation and improve aerodynamic performance. Most studies have focused on optimizing the control action for a given actuator configuration, whereas, actuator placement is intimately tied to achievable performance. In this thesis, a systematic approach for determining the optimal actuator location for separation control from numerical and experimental fluids data for both stable and unstable systems is presented. Pulse response data from high-fi...
This paper discusses an experimental study of flow separation over a 0.35 m chord NACA0015 airfoil a...
The effects of body force distribution on the control of airfoil separation flow are discussed. Stea...
3rd AIAA Flow Control Conference, San Francisco, CA, 5-8 June 2006THUNDER Piezo-cerarnic actuators w...
AIAA-03-3516, Orlando, FL, June 2003.A 2D flow control wind tunnel model was designed based on the v...
textTwo active flow control methods are investigated numerically to understand the mechanism by whic...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma ac...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma a...
This study numerically examines the effect of wall-normal momentum and vorticity injections in separ...
This paper presents the effects of airfoil geometry on flow separation behavior and obtains the tran...
This thesis addresses the problem of controlling the unsteady flow separation over an aerofoil using...
The objectives of this project are twofold: to develop a detached-eddy simulation (DES) technique fo...
Practical methods to enable control of turbulent flows in a closed-loop sense are devel-oped with a ...
Active Unsteady Flow Control experiments were performed on a Natural Laminar Flow, NLF 0414 airfoil ...
The aim of this study is to develop closed-loop feedback control algorithms for turbulent flow separ...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasm...
This paper discusses an experimental study of flow separation over a 0.35 m chord NACA0015 airfoil a...
The effects of body force distribution on the control of airfoil separation flow are discussed. Stea...
3rd AIAA Flow Control Conference, San Francisco, CA, 5-8 June 2006THUNDER Piezo-cerarnic actuators w...
AIAA-03-3516, Orlando, FL, June 2003.A 2D flow control wind tunnel model was designed based on the v...
textTwo active flow control methods are investigated numerically to understand the mechanism by whic...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma ac...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma a...
This study numerically examines the effect of wall-normal momentum and vorticity injections in separ...
This paper presents the effects of airfoil geometry on flow separation behavior and obtains the tran...
This thesis addresses the problem of controlling the unsteady flow separation over an aerofoil using...
The objectives of this project are twofold: to develop a detached-eddy simulation (DES) technique fo...
Practical methods to enable control of turbulent flows in a closed-loop sense are devel-oped with a ...
Active Unsteady Flow Control experiments were performed on a Natural Laminar Flow, NLF 0414 airfoil ...
The aim of this study is to develop closed-loop feedback control algorithms for turbulent flow separ...
We address the problem of controlling the unsteady flow separation over an aerofoil, using plasm...
This paper discusses an experimental study of flow separation over a 0.35 m chord NACA0015 airfoil a...
The effects of body force distribution on the control of airfoil separation flow are discussed. Stea...
3rd AIAA Flow Control Conference, San Francisco, CA, 5-8 June 2006THUNDER Piezo-cerarnic actuators w...