Abstract
This work aims to increase a slender structure's load-carrying capacity above its buckling point by introducing small imperfections, informed by post-buckling analysis of the unperturbed structure, known as 'modal nudging'. Specifically, we focus on structures with constrained geometry, such as wing panels, exemplified through a case study on Roorda frames.
| Original language | English |
|---|---|
| Title of host publication | ICAS PROCEEDINGS 34th Congress of the International Council of the Aeronautical Sciences |
| Publisher | International Council of the Aeronautical Sciences |
| Chapter | 04.2 |
| Number of pages | 10 |
| Publication status | Published - 8 Oct 2024 |
| Event | 34th Congress of the International Council of the Aeronautical Sciences: ICAS - Florence, Italy Duration: 9 Sept 2024 → 13 Sept 2024 https://www.icas.org/icas_archive/icas2024/index.html |
Publication series
| Name | ICAS proceedings |
|---|---|
| Publisher | International Council of the Aeronautical Sciences |
| ISSN (Electronic) | 2958-4647 |
Conference
| Conference | 34th Congress of the International Council of the Aeronautical Sciences |
|---|---|
| Country/Territory | Italy |
| City | Florence |
| Period | 9/09/24 → 13/09/24 |
| Internet address |
Research Groups and Themes
- CoSEM
Keywords
- Bifurcations
- Well-behaved nonlinear structures
- Modal nudging
- Shape optimisation
- Mode switching
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