ProfileI obtained my Master?s degree in Aerospace Engineering from the Politecnico di Torino in July 2026. Recently, I completed my Master?s thesis at the Fluid Dynamics Lab at Siemens Energy in Finspång, Sweden. My studies provided me with a solid foundation in theoretical and experimental aerodynamics, as well as proficiency in programming and CAD modeling. While working on my thesis, I was able to further develop these skills and familiarize myself with new tools and experimental methods. Motivated to contribute to innovative projects in the aerospace and energy sectors, I bring strong problem-solving skills (gained through experimental laboratory work), the ability to work effectively in a team (developed through collaboration with colleagues and supervisors), and the precision and discipline required to meet deadlines and complete tasks (shaped by 17 years of experience in football). I look forward to learning from my colleagues and contributing to challenging projects.
Technical Skills- Simulation Tools
- XFOIL
- Athena Vortex Lattice AVL
- STAR-CCM+
- FLIR ResearchIR
- RigVIEW
- C3D
- CAD Software
- Other
- Microsoft Office Suite
- LaTeX
Soft Skills- Punctual, organized, and goal-oriented
- Strong team collaboration and communication skills
- Resilient under pressure and stress management
- Passionate about sport and physical well-being
Academic Experience- CFD practice sessions using StarCCM+. The main goals during these hours were the geometry?s creation, physical model?s creation and mesh preparation in order to run different CFD calculations and analyze the results obtained. The topics covered were:
- Analysis of an incompressible flow
- Analysis of a transonic and supersonic NACA airfoil applying mesh refinement to better show shock waves and airfoil?s turbulent wake
- Analysis of an hypersonic re-entry capsule
- Preliminary design of a 100-passenger civil aircraft. In this group project the goal was to produce a preliminary aircraft concept while meeting the design requirements. The main activities in wich I was involved were:
- Aerodynamic optimization of the wing airfoil using X-foil by creating the aerodynamic polar plots and the performance plots of the airfoil
- CAD modelling of the wing shape, horizontal stabilizer and the rudder
- Static and dynamic stability evaluation of the whole aircraft configuration (fuselage, wing, control?s surfaces) using AVL
- Post processing of the analysis using Matlab
- Others responsabilities included the aircraft engine performance assesment, optimisation process, structural analysis and life fatigue analysis using analytical approach.