AIAA 2006-1387 Effects of Installation on Dynamic Pressure Measurements
Delay of Vortex Breakdown over a Delta Wing via Near-Core Blowing
High Angle of Attack Flight Control of Delta Wings Using Vortex Actuators
Combustion Instabilities and Control of a Multi-Swirl Atmospheric Combustor
AIAA 2006-1281 Dynamics of Single and Twin Circular Jets in Cross Flow
AIAA 2006-0807 Reacting and Non-Reacting Flow Fields of a V-gutter Stabilized Flame
Characterization of Blow Out Limits for a V-Gutter Stabilized Flame
Broadband Shock Associated Noise Suppression by Chevrons (AIAA2006-0009)
AIAA 2006-0907 Coherent Structures in Circular and Non-Circular Jets in Crossflow
Synchronized Acoustic Excitation of Fuel and Oxidizer for Efficient Combustion
Flow-Structure Interaction Effects on a Jet Emanating from a Flexible Nozzle (AIAA 2006-4082)
Noise Reduction by Interaction of Flexible Filaments with an Underexpanded Supersonic Jet