Nonlinear Modeling and Aeroelastic Analysis of an Adaptive Camber Wing
Author:
Affiliation:
1. Middle East Technical University, Ankara 06531, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C000312
Reference24 articles.
1. Realization of an optimized wing camber by using formvariable flap structures
2. Aerodynamic benefits of adaptive wing technology
3. Aerodynamic and aeroelastic amplification in adaptive belt-rib airfoils
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