Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing-Edge Flaps
Author:
Affiliation:
1. Swansea University, Swansea, Wales SA1 8EN, United Kingdom
Funder
Engineering and Physical Sciences Research Council
Horizon 2020 Framework Programme
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059606
Reference35 articles.
1. A Review of Morphing Aircraft
2. Performance Comparison between Optimised Camber and Span for a Morphing Wing
3. ParkerH. “The Parker Variable Camber,” NACA TR 77, 1920.
4. Design and application of compliant mechanisms for morphing aircraft structures
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