A Multi-Objective Flight Control Approach for Performance Adaptive Aeroelastic Wing
Author:
Affiliation:
1. NASA Ames Research Center
2. Delft University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1843
Reference16 articles.
1. Elastically Shaped Wing Optimization and Aircraft Concept for Improved Cruise Efficiency
2. A Mission Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift to Drag Ratios of Future N+3 Transport Aircraft
3. Experimental Investigation of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap Design
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