The design, construction, and tests of a concept aeroelastic wind tunnel model of a high-lift variable camber continuous trailing edge flap (HL-VCCTEF) wing configuration
Author:
Affiliation:
1. University of Washington, Seattle
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1406
Reference10 articles.
1. Review of State of Art of Smart Structures and Integrated Systems
2. Future of Airplane Aeroelasticity
3. A Mission Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift to Drag Ratios of Future N+3 Transport Aircraft
4. Initial Assessment of a Variable-Camber Continuous Trailing-Edge Flap System for Drag-Reduction of Non-Flexible Aircraft in Steady-State Cruise Condition
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