Transition Determination on a Periodic Pitching Airfoil Using Phase Averaging of Pressure Data
Effect of the Model-Sidewall Connection for a Static Airfoil Experiment
Effect of the Model-Sidewall Connection for a Static Airfoil Experiment
Numerical investigation of air jets for dynamic stall control on the OA209 airfoil
2008-01-0123 Scheduling Analysis and Optimization for Safety-Critical Automotive Systems
Unsteady Boundary Layer Transition Detection by Automated Analysis of Hot Film Data
Experimental investigation of high-pressure pulsed blowing for dynamic stall control
Experimental investigation of high-pressure pulsed blowing for dynamic stall control
Experimental investigation of high-pressure pulsed blowing for dynamic stall control
Air force crew numbers to be cut by 40% as service adopts revised operational-command structure
Boundary Layer Transition Measurements on Hovering Helicopter Rotors by Infrared Thermography