Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Flutter Analysis of the Transonic Truss-Braced Wing Aircraft Using Transonic Correction
2012-3250 Flow Control by Pulsed Jet in a Highly Bended S-duct
2012-3138 Shear Layer Characteristics of the Supersonic Free and Impinging Jets
2012-3043 Interaction of a Single Synthetic Jet with a Finite Aspect Ratio Circular Cylinder
2012-2958 Investigation and Active Control of Bluff Body Vortex Shedding Using Plasma Actuators
2012-2812 Comparison of Micro-Vortex Generators in Supersonic Flows
2012-3245 High-Lift Enhancement Using Active Flow Control
2012-2945 Transition Delay Using DBD Plasma Actuators in Direct Frequency Mode
2012-2682 Control of Laminar Separation Bubble Using Electro-Active Polymers
2012-3248 Effect of Microjet-Spacing on the Control of a Highly Separated Flowfield
2012-3237 Characterization of Corner Plasma Actuators for Pulsed Jet Production
2012-2952 Active Control of a Wing Tip Vortex with a Dielectric Barrier Discharge Plasma Actuator
2012-2810 Control of Oblique Shock Wave-Boundary Layer Interactions Using Plasma Actuators
2012-2806 Slat Noise Feedback Control with a Dielectric Barrier Discharge Plasma Actuator