Dynamic Aeroelastic Response Attenuation of Aerospace Structures Employing Passive Tuned Mass Dampers
Public Deposited- Resource Type
- Creator
- Abstract
This thesis proposes an optimization procedure to achieve the best configuration of multiple degrees of freedom tuned mass dampers (TMD) to mitigate the global dynamic aeroelastic response of aerospace structures. The TMD design parameters are investigated in terms of their individual mass, stiffness, damping, and location on the target structure. In order to determine the optimum sets of TMD, a multi-objective design optimization employing a genetic algorithm is implemented, where the selected fitness functions for the analysis are the minimization of the total mass included with the resonators and concurrent minimization of the peak displacement at specific structural nodes. Two case studies are presented, where the method is tested to minimize the pointing error of large Earth-based radio antennas. Fourteen operational scenarios of wind gust are considered, employing two models of atmospheric disturbances, where the dynamic aeroelastic response of the structure is analyzed in the frequency and the time domains.
- Subject
- Language
- Publisher
- Thesis Degree Level
- Thesis Degree Name
- Thesis Degree Discipline
- Identifier
- Rights Notes
Copyright © 2021 the author(s). Theses may be used for non-commercial research, educational, or related academic purposes only. Such uses include personal study, research, scholarship, and teaching. Theses may only be shared by linking to Carleton University Institutional Repository and no part may be used without proper attribution to the author. No part may be used for commercial purposes directly or indirectly via a for-profit platform; no adaptation or derivative works are permitted without consent from the copyright owner.
- Date Created
- 2021
Relations
- In Collection:
Items
Thumbnail | Title | Date Uploaded | Visibility | Actions |
---|---|---|---|---|
gasparetto-dynamicaeroelasticresponseattenuationofaerospace.pdf | 2023-05-05 | Public | Download |