2012-2805 Transient Aerodynamic Response to Leading Edge Flow Control
2012-3052 Unsteady Forcing of a Post-Stall Flow Over a NACA0012 Airfoil by a Surface DBD Actuator
2012-2955 The Transient Response of a von Karman Ogive to Open Loop Plasma Actuation
2012-2802 Multivariable Closed-Loop Flow Control of Drag and Yaw Moment for a 3D Bluff Body
2012-3251 A New Linear High Speed Compressor Stator Cascade for Active Flow Control Investigations
2012-3246 Aerodynamic Control Using Distributed Bleed
2012-2681 Low Reynolds Number Airfoil Stall Suppression with Dynamic Roughness
2012-3135 Combustion Powered Actuators for Separation Control (Invited)
2012-2956 Plasma Control for a Maneuvering Low-Aspect-Ratio Wing at Low Reynolds Number
2012-2953 Vortex Dynamics of a Tangent Ogive at High Angle of Attack
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