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

https://doi.org/10.2139/ssrn.5087737
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Liquid hydrogen fuel tanks for commercial aviation: Structural sizing and stress analysis
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Greenhouse gas emissions assessment of hydrogen and kerosene-fueled aircraft propulsion
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Hydrogen fuel tanks for subsonic transport aircraft
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Life cycle evaluation of hydrogen and other potential fuels for aircrafts
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Hydrogen as the fuel of the future in aircrafts – Challenges and opportunities
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Conceptual design and optimization of a general aviation aircraft with fuel cells and hydrogen
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Performance and failure analysis of a retrofitted Cessna aircraft with a Fuel Cell Power System fuelled with liquid hydrogen
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Conceptual design of hybrid-electric transport aircraft
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Aviation gas turbine alternative fuels: A review
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Science and technology of ammonia combustion
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Comparative life cycle evaluation of alternative fuels for a futuristic subsonic long-range aircraft
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Biofuels in aviation: Fuel demand and CO2 emissions evolution in Europe toward 2030
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Energy performance evaluation of alternative energy vectors for subsonic long-range tube-wing aircraft
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The historical fuel efficiency characteristics of regional aircraft from technological, operational, and cost perspectives
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A Model for the Prediction of Thermal, Prompt, and Fuel NOx Emissions From Combustion Turbines
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Hydrogen Aircraft Technology
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A review on potential use of hydrogen in aviation applications
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Benefits and challenges of liquid hydrogen fuels in commercial aviation
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Design and Optimisation of Fuel Tanks for BWB Configurations
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Systems Evaluation of Subsonic Hybrid-Electric Propulsion Concepts for NASA N+3 Goals and Conceptual Aircraft Sizing
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Hybrid-Electric Propulsion for Aircraft
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Aircraft Engine Design, Third Edition
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Conceptual Design of a Hydrogen-Propelled Aircraft with Distributed Electric Propulsion
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An Approach to Evaluate Fleet Level CO2 Impact of Introducing Liquid-Hydrogen Aircraft to a World-Wide Network
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Data in Brief : Performance Sensitivity of Subsonic Liquid Hydrogen Long-Range Tube-Wing Aircraft to Technology Developments
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Data in Brief : Conceptual Design-Optimisation of Futuristic Hydrogen Powered Ultrahigh Bypass Ratio Geared Turbofan Engine
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