Performance Enhancement of Tilt-Rotor Unmanned Aerial Vehicle Using Nacelle-Fixed Auxiliary Wing
Author:
Affiliation:
1. School of Mechanical, Aerospace and Systems Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031896
Reference9 articles.
1. NixonM. W. “Improvements to Tilt Rotor Performance Through Passive Blade Twist Control,” NASA TM-100583, 1988.
2. Demonstration of an elastically coupled twist control concept for tilt rotor blade application
3. OzbayS. “Extension-Twist Coupling Optimization in Composite Rotor Blades,” Ph.D. Dissertation, School of Aerospace Engineering, Georgia Inst. of Technology, Atlanta, 2006.
4. Design of a variable twist tilt-rotor blade using shape memory alloy (SMA) actuators
5. Design and analysis of variable-twist tiltrotor blades using shape memory alloy hybrid composites
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