2012-2737 On Gasdynamic Instabilities Supported by Non-Equilibrium Plasma in a Supersonic Flow
2012-2801 Flight and Wind Tunnel Tests of Closed-Loop Active Flow Control
2012-2802 Multivariable Closed-Loop Flow Control of Drag and Yaw Moment for a 3D Bluff Body
2012-2803 Closed-Loop Performance Control of DBD Plasma Actuators
2012-2804 Active Flow Control of a Pitching Turret Flow Field Using Closed-Loop Feedback Control
2012-2805 Transient Aerodynamic Response to Leading Edge Flow Control
2012-2806 Slat Noise Feedback Control with a Dielectric Barrier Discharge Plasma Actuator
2012-2807 Simultaneous Drag Reduction and Kinetic Energy Density of the Plane Poiseuille Flow
2012-2808 Detection and Transient Dynamics Modeling of Experimental Hypersonic Inlet Unstart
2012-2809 Experimental Study and Plasma Control of an Unstarting Supersonic Flow
2012-2810 Control of Oblique Shock Wave-Boundary Layer Interactions Using Plasma Actuators
2012-2811 Adjoint Optimization of Mass, Momentum and Energy Addition in Steady Supersonic Flow
2012-2812 Comparison of Micro-Vortex Generators in Supersonic Flows
2012-2813 Experiments on Resonance Enhanced Pulsed Microjet Actuators in Supersonic Crossflow
2012-2814 SparkJet Actuator Characterization in Supersonic Cross Flow
2012-2945 Transition Delay Using DBD Plasma Actuators in Direct Frequency Mode