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Title: Aerostructural Wing and Fuselage Optimization for Hydrogen-based Aircraft
Background: Currently, aviation is undergoing a large shift towards more sustainable, eco-friendly, and efficient aviation to meet the International Air Transport Association (IATA) ambitious
Background: Currently, aviation is undergoing a large shift towards more sustainable, eco-friendly, and efficient aviation to meet the International Air Transport Association (IATA) ambitious
targets to mitigate CO2 emissions by 50% from air transport until 2050. Hydrogen technologies have emerged as a potential energy source represent a long-term option as a fuel for aviation. Beyond the purely technological issues, a holistic assessment requires looking at the
integration of hydrogen into the aircraft design towards hydrogen-powered aircraft. The development of the necessary systems to store and distribute hydrogen fuel on the aircraft for flight is a mandatory step toward such a system. Since liquid hydrogen cannot be reasonably
