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
2012-2948 Interaction of a Finite-Span Synthetic-Jet and a Cross-Flow over a Sweptback Finite Wing
2012-2949 Efficiency of Slotted Jet Actuators at High Subsonic Mach Numbers
2012-2951 Experimental Studies of DBD Actuator Effects on Wing Tip Vortex Topology
2012-2952 Active Control of a Wing Tip Vortex with a Dielectric Barrier Discharge Plasma Actuator
2012-2953 Vortex Dynamics of a Tangent Ogive at High Angle of Attack
2012-2955 The Transient Response of a von Karman Ogive to Open Loop Plasma Actuation
2012-2956 Plasma Control for a Maneuvering Low-Aspect-Ratio Wing at Low Reynolds Number
2012-2958 Investigation and Active Control of Bluff Body Vortex Shedding Using Plasma Actuators