Hydrogen-Powered Aircraft: Concepts, Technologies, and Environmental Impact - presented by Prof. Joaquim R. R. A. Martins FRAeS, FAIAA

Hydrogen-Powered Aircraft: Concepts, Technologies, and Environmental Impact

Prof. Joaquim R. R. A. Martins FRAeS, FAIAA

Prof. Joaquim R. R. A. Martins FRAeS, FAIAA

Associated Progress in Aerospace Sciences article

E. J. Adler and J. R. R. A. Martins (2023) Hydrogen-powered aircraft: Fundamental concepts, key technologies, and environmental impacts. Progress in Aerospace Sciences
Article of record
Hydrogen-Powered Aircraft: Concepts, Technologies, and Environmental Impact
Prof. Joaquim R. R. A. Martins FRAeS, FAIAA
Joaquim R. R. A. Martins
University of Michigan–Ann Arbor

Civil aviation has an outsized social and economic influence and is indispensable in the global economy. However, aircraft have a negative impact on the environment. Society needs revolutionary aircraft technology to meet environmental goals and sustain the civil aviation industry. Hydrogen aircraft have the potential to fly existing routes with no carbon emissions and reduce or eliminate other emissions. In the long term, hydrogen aircraft appear to be the most compelling alternative to today's kerosene-powered aircraft. Using hydrogen also enables novel technologies, such as fuel cells and superconducting electronics, which could lead to aircraft concepts that are not feasible with kerosene. Hydrogen aircraft introduce technical challenges. While they appear technically feasible, they require further development of hydrogen storage tanks, fuel systems, and propulsion technologies.

References
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    E. J. Adler and J. R. R. A. Martins (2023) Hydrogen-powered aircraft: Fundamental concepts, key technologies, and environmental impacts. Progress in Aerospace Sciences
  • 2.
    B. J. Brelje and J. R. R. A. Martins (2018) Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches. Progress in Aerospace Sciences
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    E. J. Adler et al. (2022) Thermal Management System Optimization for a Parallel Hybrid Aircraft Considering Mission Fuel Burn. Aerospace
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  • 6.
    J. L. Anibal et al. (2022) Aerodynamic shape optimization of an electric aircraft motor surface heat exchanger with conjugate heat transfer constraint. International Journal of Heat and Mass Transfer
  • 7.
    Z. Lyu and J. R. R. A. Martins (2014) Aerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft. Journal of Aircraft
  • 8.
    J. R. R. A. Martins (2022) Aerodynamic design optimization: Challenges and perspectives. Computers & Fluids
  • 9.
    J. R. R. A. Martins and G. J. Kennedy (2021) Enabling large-scale multidisciplinary design optimization through adjoint sensitivity analysis. Structural and Multidisciplinary Optimization
Grants
    Glenn Research CenterNASA award 80NSSC18M0151
Brahmal Vasudevan Institute for Sustainable Aviation logo
Brahmal Vasudevan Institute for Sustainable Aviation Seminar Series
Brahmal Vasudevan Institute for Sustainable Aviation (Imperial College London)
Cite as
J. R. R. A. Martins (2023, March 7), Hydrogen-Powered Aircraft: Concepts, Technologies, and Environmental Impact
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Video length 59:23
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