AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
DIGITAL TWIN APPROACH FOR STRUCTURAL PROPERTY EVALUATION OF NEXT GENERATION ACTIVE TWIST BLADES
Hybrid Integrated Microphotonics and It's Applications
A Fast-Response Probe Capable of Atmospheric Sampling in Harsh Conditions (AIAA 2013-4668)
Experimental Study on the Near Field Structure of Wing-Tip Vortex
ICE ACCRETION EFFECT ON THE AERODYNAMIC CHARACTERISTICS OF KC-100 AIRCRAFT
An examination of the maneuverability of an all wheel steer vehicle at low speed
AIAA-2004-5190 Numerical Simulation of the Three-Dimensional Flow for Flush Inlet
Helicopter Vibration Reduction Using Active Twist Control of Composite Rotor Blades
Enabling Operational Autonomy for UAVs with Robustness (AIAA 2013-4652)
Increasing Operational and Fuel Efficiency for Multi-UAV Missions (AIAA 2013-4732)
A Refined Structural Dynamics Model for Composite Rotor Blades
Genetic Algorithm for the Time-Dependent Vehicle Routing Problem
AIAA-2003-3938 Investigation of Plume Effects on Longitudinal Aerodynamics of Missile at M=1.2
Absolute Orientation for a UAV using Celestial Objects (AIAA 2013-5145)
Numerical Modeling for Eulerian Droplet Impingement in Supercooled Large Droplet Conditions