Flutter Analysis of a Morphing Wing Considering Fluid–Thermal–Structure Coupling
Tianxing Chen, Kun Guo, Huichao Deng, Yuchen Xia, Hao Luo, Yunlong Li +1 · American Institute of Aeronautics and Astronautics (AIAA) · 2026
This study conducts a flutter analysis of morphing wings, revealing critical insights into stability under varying conditions.
Plain English summary
Why this matters
Key findings
- Flutter onset is governed by the coupling of the first two structural modes.
- A secondary instability pathway emerges for the fully extended wing.
- Critical flutter speed is degraded by increasing temperature and geometric extension.
- Flutter frequency has a non-monotonic relationship with the extension ratio.
- The findings provide a framework for the design and control of morphing aircraft.
What's new
The study systematically evaluates the coupled effects of fluid dynamics, thermal loading, and structural deformation on morphing wings.
Limitations
The abstract does not specify experimental validation or real-world application scenarios.
Commercial context
The abstract does not provide information on commercial applications or readiness.
Publication
- Publisher
- American Institute of Aeronautics and Astronautics (AIAA)
- Publication date
- August 1, 2026
- Research type
- Paper
Tags
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