Print Email Facebook Twitter Aircraft Design Optimization Considering Network Demand and Future Aviation Fuels Title Aircraft Design Optimization Considering Network Demand and Future Aviation Fuels Author Proesmans, P. (TU Delft Flight Performance and Propulsion) Morlupo, F. (TU Delft Air Transport & Operations) Santos, Bruno F. (TU Delft Air Transport & Operations) Vos, Roelof (TU Delft Flight Performance and Propulsion) Date 2023 Abstract To reduce the climate impact of aviation, researchers are studying the replacement of fossil kerosene with liquid hydrogen and/or drop-in sustainable aviation fuel (SAF). These fuels can bring significant reductions in CO2 emissions and can offer savings in terms of non-CO2 climate effects. In addition, tube-and-wing aircraft can be optimized to decrease the global-warming impact by using a climate metric as a design objective rather than the operating costs. Previous research has shown that airplanes designed for minimal climate impact have a reduced cruise speed and fly at a lower altitude. This paper suggests a multidisciplinary, multi-level approach the evaluate the consequences of such design and fuels choices at the network level. Following the aircraft design step, a dynamic programming routine allocates the fleet and schedules the flights to maximize the network profit. We consider a hub-and-spoke network operating from Atlanta, with demand for domestic and international destinations. Compared to the reference cost-optimal kerosene fleet, a fleet consisting of climate-optimized kerosene aircraft can reduce the climate impact by 61% at a loss in network profit of approximately 21%. This design choice requires allocating an additional five aircraft. A fleet operating climate-optimal, hydrogen aircraft minimizes the climate impact. However, the high operating cost of long-range, hydrogen aircraft lowers the achievable profit. Aircraft powered by drop-in SAF provides Pareto-optimal solutions. These insights can be used to make decisions about the allocation of future aviation fuels in a network and the payload-range requirements of future aircraft. Subject Aircraft DesignMDOClimate ImpactAircraft OperationsHydrogen Aircraft To reference this document use: http://resolver.tudelft.nl/uuid:242cba3c-236b-4fc3-8e83-047b9ed0c042 DOI https://doi.org/10.2514/6.2023-4300 Publisher American Institute of Aeronautics and Astronautics Inc. (AIAA) ISBN 978-1-62410-704-7 Source AIAA AVIATION 2023 Forum Event AIAA AVIATION 2023 Forum, 2023-06-12 → 2023-06-16, San Diego, United States Part of collection Institutional Repository Document type conference paper Rights © 2023 P. Proesmans, F. Morlupo, Bruno F. Santos, Roelof Vos Files PDF 6.2023_4300.pdf 789.67 KB Close viewer /islandora/object/uuid:242cba3c-236b-4fc3-8e83-047b9ed0c042/datastream/OBJ/view