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handle: 2117/393108
This is a project whose main objective is to determine the required values of thrust, power, and efficiency for the propulsion systems of the ONA DLC eVTOL aircraft by ONAerospace during the hover and cruise phases. Additionally, it is an investigation work on both open propeller and ducted fan propulsion systems.
Objectius de Desenvolupament Sostenible::9 - Indústria, Innovació i Infraestructura
Objectius de Desenvolupament Sostenible::11 - Ciutats i Comunitats Sostenibles
Batteries, Vehicles espacials--Sistemes de propulsió, Hydrogen cell, Rotor, Tiltrotor, EVTOL, Propeller, Electric engine, Multirotor, Hydrogen cell., Ducted fan, Space vehicles--Propulsion systems, Àrees temàtiques de la UPC::Aeronàutica i espai::Sistemes de propulsió
Batteries, Vehicles espacials--Sistemes de propulsió, Hydrogen cell, Rotor, Tiltrotor, EVTOL, Propeller, Electric engine, Multirotor, Hydrogen cell., Ducted fan, Space vehicles--Propulsion systems, Àrees temàtiques de la UPC::Aeronàutica i espai::Sistemes de propulsió
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