Hybrid Integrated Microphotonics and It's Applications
An Aerodynamic Shape Optimization Study to Maximize the Range of a Guided Missile
An Aerodynamic Shape Optimization Study to Maximize the Range of a Guided Missile
AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
Camera trajectory estimation using inertial sensor measurements and structure from motion results
Camera Trajectory Estimation Using Inertial Sensor Measurements and Structure from Motion Results
AIAA-2004-5190 Numerical Simulation of the Three-Dimensional Flow for Flush Inlet
An examination of the maneuverability of an all wheel steer vehicle at low speed
Experimental Study on the Near Field Structure of Wing-Tip Vortex
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)
Helicopter Vibration Reduction Using Active Twist Control of Composite Rotor Blades
Increasing Operational and Fuel Efficiency for Multi-UAV Missions (AIAA 2013-4732)
Enabling Operational Autonomy for UAVs with Robustness (AIAA 2013-4652)
DIGITAL TWIN APPROACH FOR STRUCTURAL PROPERTY EVALUATION OF NEXT GENERATION ACTIVE TWIST BLADES
A Refined Structural Dynamics Model for Composite Rotor Blades