M.Sc. Thesis concluded: “Aeroelastic study of aircraft with box-wing architecture using a medium-low fidelity code”

After a 6 months internship at XSun (France), the student Andri Dine has concluded a M.Sc. thesis aimed at evaluating the capabilities of a low fidelity aeroelastic tool in defining the aero-structrual behaviour of box-wing aircraft since the early stages of the design. Reference: Dine, A., “Studio aeroelastico di velivoli con architettura box-wing mediante un […]

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A new paper published in Applied Sciences (MDPI): “A Conceptual Design Methodology for e-VTOL Aircraft for Urban Air Mobility” (Open Access)

Recent progress of electric systems has raised attention towards hybrid-electric and full-electric aircraft. Nevertheless, the current low battery energy density limits the application of these propulsive architectures to large transport aircraft. In the context of the general aviation category, full-electric aircraft for the so-called Urban Air Mobility scenario are gaining increasing interest. These air taxis, […]

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