Abstract
This research utilizes a Multi-Mass Tuned Mass Damper (MMTMD) system to effectively control aeroelastic vibrations in aircraft wings. Unstable aerodynamic forces such as lift and drag can cause aircraft wings with broad cantilever spans and inadequate stiffness to oscillate at low frequencies, particularly in their fundamental mode. A distinctive passive dampening system featuring numerous slender metallic bars linked to separate masses and strategically integrated into the wing structure effectively tackles this challenge. In contrast to single-mass Tuned Mass Dampers, these components address both fundamental and higher-order vibration modes, enhancing damping effectiveness across a broader frequency spectrum. Simulations utilizing the Finite Element Method (FEM) have been benchmarked against established reference findings, confirming the effectiveness of the system. The proposed MMTMD achieved a remarkable reduction in peak displacement amplitudes by 72.2 % (from ±90 mm to ±25 mm), while traditional TMDs managed a decrease of only 55.5 % (±40 mm). The results highlight the exceptional capability of the MMTMD in reducing structural vibrations. The research indicates that MMTMD enhances vibration attenuation in real aerodynamic stress conditions, thereby prolonging the structural integrity and operational lifespan of aircraft wings. The findings are consistent with the principles outlined by Magalhães et al. (2023), showcasing the efficacy of multi-mass damping techniques in complex dynamic systems.
| Original language | English |
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| Title of host publication | Proceedings of ASME 2025 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, SMASIS 2025 |
| Publisher | American Society of Mechanical Engineers (ASME) |
| ISBN (Electronic) | 9780791889275 |
| DOIs | |
| State | Published - 2025 |
| Event | 18th Annual Conference of the Smart Materials, Adaptive Structures and Intelligent Systems, SMASIS 2025 - St. Louis, United States Duration: 8 Sep 2025 → 10 Sep 2025 |
Publication series
| Name | Proceedings of ASME 2025 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, SMASIS 2025 |
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Conference
| Conference | 18th Annual Conference of the Smart Materials, Adaptive Structures and Intelligent Systems, SMASIS 2025 |
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| Country/Territory | United States |
| City | St. Louis |
| Period | 8/09/25 → 10/09/25 |
Bibliographical note
Publisher Copyright:Copyright © 2025 by ASME.
Keywords
- FEM
- Multi-Mass TMD
- aircraft wings
- multi-mode vibration
- passive control
ASJC Scopus subject areas
- Artificial Intelligence
- Civil and Structural Engineering
- Mechanics of Materials