A flexible sandwich structure skin for camber morphing wing
P.N. Gautham Vigneswar, Shaikh Faruque Ali, A. Arockiarajan · SAGE Publications · 2025
This study presents a flexible sandwich structure skin for wing morphing, showcasing a novel assembly technique and successful prototype demonstration.
Plain English summary
Why this matters
Key findings
- The flexible sandwich structure skin can withstand large bending deflections.
- The novel self-adjusting assembly technique integrates well with internal morphing mechanisms.
- Experimental evaluations confirm the skin's durability without failure.
- Finite element simulations assess operational stresses and deformations.
- A working prototype has been fabricated and demonstrated.
What's new
The introduction of a self-adjusting assembly technique for integrating morphing mechanisms is a new contribution.
Limitations
The abstract does not provide details on the long-term performance or scalability of the proposed skin.
Commercial context
The prototype has been demonstrated, indicating potential for further development and application in the aerospace industry.
Publication
- Publisher
- SAGE Publications
- Publication date
- September 23, 2025
- Research type
- Paper
- License
- https://journals.sagepub.com/page/policies/text-and-data-mining-license
Tags
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