Self-adaptive morphing wing model, smart actuated and controlled by using a multiloop controller based on a laminar flow real time optimizer
Author:
Affiliation:
1. University of Québec
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-1082
Reference33 articles.
1. Morphing Airfoil Shape Change Optimization With Minimum Actuator Energy As An Objective
2. Optimization of a Morphing Wing Based on Coupled Aerodynamic and Structural Constraints
3. Active flow control based on transonic design concepts
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