Rotorcraft

Experimental and Numerical Analysis of Unsteady Rotating and Flapping Multi-Wing Systems
PhD thesis in Aerospace Engineering.
Development of numerical models for coaxial rotors (BEMT + UVLM) and tandem flapping wings (UVLM), with experimental validation.
Thomas Lambert
Project Project Project
Experimental and Numerical Analysis of Unsteady Rotating and Flapping Multi-Wing Systems
Rotare
A feature-rich and Open-Source implementation of the BEMT in Matlab
Rotare