Comparison of Velocities Driven by Repetitive Nanosecond Pulses to AC Result (AIAA 2014-0327)
Flow Control over a Conical Forebody Using Pulsed Nanosecond Discharge Actuators (AIAA 2014-0933)
Comparison of Pressures Driven by Repetitive Nanosecond Pulses to AC Result (AIAA 2014-0094)
Nonpremixed Combustion in an Accelerating Turning Transonic Flow Undergoing Transition AIAA Paper
Euler Solutions of Flow Around a Rectangular Wing with Square Tip AIAA Paper
Aerodynamic Characteristics of Slender Delta Wing with Low Dorsal Fin AIAA Paper
Computational Analysis of Conical Forebody at High Angles of Attack with Transitional Model
AIAA 2006-1055 Optimization of Unstalled Pitching and Plunging Motion of an Airfoil
Supercritical Flow over Unstalled Plunging Airfoil Computed by Euler Method (AIAA 2006-0293)
Investigation of NACA 0012 Airfoil Periodic Flows in a Transonic Wind Tunnel
PIV Study of Conical Forebody Flow Control Using Plasma Actuators
Optimal DBD Duty-Cycle for Conical Forebody Side-Force Proportional Control
Experimental Study of DBD Plasma Actuation Body Force Based on PIV
An Experimental Study of the Rudimentary Landing Gear
Analysis of the Effects of Wall Interference on 0.4x0.8-Meter Transonic Wind Tunnel Airfoils Tests
Experimental Study of Shock Wave Oscillation on SC(2)-0714 Airfoil
Body Force Produced by Plasma Actuator Using PIV and Pressure Measurements
Flow Control over Conical Forebody with Port Pulsed Plasma Actuator