Hybrid Integrated Microphotonics and It's Applications
AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
Experimental Study on the Near Field Structure of Wing-Tip Vortex
AIAA-2004-5190 Numerical Simulation of the Three-Dimensional Flow for Flush Inlet
Helicopter Vibration Reduction Using Active Twist Control of Composite Rotor Blades
Passenger airline choice behavior for domestic short-haul travel in South Korea
A Fast-Response Probe Capable of Atmospheric Sampling in Harsh Conditions (AIAA 2013-4668)
Enabling Operational Autonomy for UAVs with Robustness (AIAA 2013-4652)
Increasing Operational and Fuel Efficiency for Multi-UAV Missions (AIAA 2013-4732)