Nonlinear Aeroelasticity of Morphing Wings with Corrugated Structures
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
2. University of Tokyo
3. University of Alabama, Tuscaloosa
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0219
Reference29 articles.
1. The X-53 A Summary of the Active Aeroelastic Wing Flight Research Program
2. Aerodynamic Flight Test Results for the Adaptive Compliant Trailing Edge
3. Longitudinal Aerodynamic Modeling of the Adaptive Compliant Trailing Edge Flaps on a GIII Aircraft and Comparisons to Flight Data
4. Development of Variable Camber Continuous Trailing Edge Flap for Performance Adaptive Aeroelastic Wing
5. Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW
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1. Recent developments in the aeroelasticity of morphing aircraft;Progress in Aerospace Sciences;2021-01
2. A combined experimental-numerical analysis of a novel deformable sandwich structure for morphing wing applications;Journal of Sandwich Structures & Materials;2020-12-10
3. Geometrically nonlinear electro-aeroelastic framework for morphing wing with piezoelectric actuators;Transactions of the JSME (in Japanese);2019
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