Files
BEGON_13801900_2025.pdf
UCLouvain restricted access - Adobe PDF
- 3.21 MB
Details
- Supervisors
- Faculty
- Degree label
- Abstract
- Fluid–structure interaction is a complex phenomenon that occurs widely and continually, all around us. To better understand and predict aeroelastic behavior, appropriate numerical simulation tools are required. Some of those, although very accurate and reliable, are extremely demanding in computing time and resources. This thesis details the development, verification, and application of an unsteady, low-cost Fluid–structure interaction solver, based on the vortex-sheet method, over two-degree-of-freedom rigid airfoils. The solver enables parametric analysis, investigations of flutter and responses to disturbed environments with useful accuracy while keeping a reduced computational cost.