Optimum Wing Shape of Highly Flexible Morphing Aircraft for Improved Flight Performance
Author:
Affiliation:
1. University of Alabama, Tuscaloosa, Alabama 35487-0280
2. NASA Ames Research Center, Moffett Field, California 94035
3. Michigan State University, East Lansing, Michigan 48824
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033490
Reference23 articles.
1. Modeling of High Aspect Ratio Active Flexible Wings for Roll Control
2. Active Warping Control of a Joined Wing/Tail Airplane Configuration
3. Flight Testing of Mission Adaptive Compliant Wing
4. Novel, Bidirectional, Variable-Camber Airfoil via Macro-Fiber Composite Actuators
5. Design Optimization of a Controllable Camber Rotor Airfoil
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