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Flugmechanik
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Simulation of Flight Dynamics with an Improved Post-Stall Aerodynamics Model
A Rapid Aerodynamic Prediction Method for Simulation of Post-Stall Flight Dynamics
Unsteady and Post-Stall Aerodynamic Modeling for Flight Dynamics Simulation (AIAA 2014-0729)
Flight Test of Stable Automated Cruise Flap for an Adaptive Wing Aircraft
Experimental Investigation of Bio-Inspired High Lift Effectors on a 2-D Airfoil
Theoretical Modeling of Leading Edge Vortices Using the Leading Edge Suction Parameter
Effect of Airfoil Shape and Reynolds Number on Leading Edge Vortex Shedding in Unsteady Flows
Use of Lift Superposition for Improved Computational Efficiency of Wing Post-Stall Prediction
A Time-Lag Approach for Prediction of Trailing-Edge Separation in Unsteady Flow (AIAA 2014-2701)
AIAA-2003-3499 Incorporation of Aircraft Performance Considerations in Inverse Airfoil Design
A CFD Database for Airfoils and Wings at Post-Stall Angles of Attack
Theoretical Analysis of Perching and Hovering Maneuvers
AIAA-2004-4721 Analytical and Computational Study of Adaptive Circulation Control Airfoils
AIAA-2004-4722 Ideal Lift Distributions and Flap Angles for Adaptive Wings
Inverse Design of Adaptive Airfoils with Aircraft Performance Considerations (invited)
Systematic Airfoil Design Studies at Low Reynolds Numbers
Design of High-Lift Airfoils for Low Aspect Ratio Wings with Endplate4