Sizing and feasibility of modular structures for unmanned platforms
Thesis in external company
Reference persons MARCO GHERLONE
Research Groups 02-AESDO
Thesis type NUMERICAL
Description The objective is to investigate the structural potential and weak points of modular aeronautical platforms, composed of a "basic" aircraft structure on which to install modular payloads, based on the required mission profile.
Starting from a CAD model and the associated aerodynamic loads, the student will have to generate the FEM model with Hyperworks and carry out the related analyses.
Required skills Knowledge of FEM commercial codes
Deadline 20/12/2023 PROPONI LA TUA CANDIDATURA