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Polaris - Design of Liquid Hydrogen Turbo-Electric Transport Aircraft

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inferred← citeshttps://doi.org/10.2139/ssrn.5087737openalex-extracted

Data in Brief : Energy Performance Evaluation of Alternative Energy Vectors for Subsonic Intercontinental Tube-Wing Aircraft

inferred← citeshttps://doi.org/10.1016/j.enrev.2022.100001openalex-snapshot

Low-carbon transition in smart city with sustainable airport energy ecosystems and hydrogen-based renewable-grid-storage-flexibility

inferred← citeshttps://doi.org/10.1016/j.ijepes.2025.110551openalex-snapshot

Hydrogen–electric–thermal coupling analysis and validation of superconducting turbo-electric hybrid propulsion system

inferred← citeshttps://doi.org/10.1016/j.ijhydene.2023.03.266openalex-snapshot

Potential analysis of hydrogen storage systems in aircraft design

inferred← citeshttps://doi.org/10.1016/j.ijhydene.2023.07.297openalex-snapshot

Performance sensitivity of subsonic liquid hydrogen long-range tube-wing aircraft to technology developments

inferred← citeshttps://doi.org/10.1016/j.ijhydene.2024.10.329openalex-snapshot

Conceptual design-optimisation of a future hydrogen-powered ultrahigh bypass ratio geared turbofan engine

inferred← citeshttps://doi.org/10.1016/j.ijhydene.2024.11.331openalex-snapshot

Conceptual design-optimisation of a subsonic hydrogen-powered long-range blended-wing-body aircraft

inferred← citeshttps://doi.org/10.1016/j.paerosci.2023.100967openalex-snapshot

Thermal management challenges in hybrid-electric propulsion aircraft

inferred← citeshttps://doi.org/10.1016/j.trd.2022.103588openalex-snapshot

Energy performance evaluation of alternative energy vectors for subsonic long-range tube-wing aircraft

inferred← citeshttps://doi.org/10.1088/1742-6596/2526/1/012017openalex-snapshot

Overview and preliminary results of the Scalability Investigation of hybrid Electric concepts for Next-generation Aircraft (SIENA) project

inferred← citeshttps://doi.org/10.3390/en14216861openalex-snapshot

Barriers and Challenges Going from Conventional to Cryogenic Superconducting Propulsion for Hybrid and All-Electric Aircrafts

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