Flexible Multi-Disciplinary Design Optimisation of Novel Configurations for Hydrogen Powered Commercial Aircraft

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The purpose of this investigation is to develop a flexible method to determine the optimal configuration of next generation passenger aircraft powered by hydrogen. This will investigate the aerodynamic, structural and energy disciplines of innovative aircraft configurations by looking specifically at the aircraft layout, wing sizing, fuel storage and cabin capacity, aiming to deliver a single concept. Particular focus on contrail formation will establish the project novelty by investigating potential aircraft configurations for long range flight at high altitude. This is an area which has a significant paucity of research and contributes the highest overall emissions per passenger kilometre, 6% of long range flights are responsible for 50-75% of aircraft emissions. Fundamentally, measuring the effects of hydrogen propulsion remains an unsolved challenge and is the best target for radical and impactful optimised designs. It is the interaction of environment, propulsion and aircraft architecture which make this complex challenge relevant to future commercial aircraft design. Underpinning this is the need to develop the next generation of efficient aircraft which meet net-zero emissions targets and to ensure the long-term sustainability of air transport. Working with Airbus this research will be industry aligned and focused on current industry trends.