Effectiveness of Wing Twist Morphing in Roll Control
Author:
Affiliation:
1. University of Naples “Federico II,”, 80125 Naples, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C000328
Reference18 articles.
1. Design and Functional Test of a Morphing High-Lift Device for a Regional Aircraft
2. Airfoil Structural Morphing Based on S.M.A. Actuator Series: Numerical and Experimental Studies
3. Adaptive wing and flow control technology
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