Published September 24, 2024
| Version 1.0.0
Presentation
Open
A FEM-based morphing wing concept with periodic cell metamaterial outer surface
Authors/Creators
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1.
Brno University of Technology
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2.
Imperial College London
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3.
Trencianska Univerzita Alexandra Dubceka V Trencine
Description
Morphing wings have a significant impact of aircraft performance in different flight phases. The outer surface of the leading edge is subjected to large deflections leading to large stresses when considering standard materials and structures. The initial requirement of the morphing is that the additional weight of the structure, i.e. kinematic mechanism, should not prevail the benefits of the effect to the aerodynamic performance of the wing. Thus, integrating of metamaterial structures with functionally
graded characteristics is beneficial to control bending and axial stiffness while fulfilling the weight limitations.
Files
Hrstka_M_MSE2024.pdf
Files
(5.6 MB)
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Additional details
Funding
Dates
- Available
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2024-09-24
Software
- Programming language
- Python