Review of hybrid-electric aircraft technologies and designs: Critical analysis and novel solutions
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H. Zhang, C. Saudemont, B. Robyns, M. Petit, Comparison of technical features between a More Electric Aircraft and a Hybrid Electric Vehicle, in: IEEE Conference on Vehicle Power and Propulsion, 3–5 September, VPPC, Harbin, China, 2008, pp. 1–6, http://dx.doi.org/10.1109/VPPC.2008.4677663.
McNutt, 2013, Climate change impacts, Science, 341, 435, 10.1126/science.1243256
Lee, 2009, Aviation and global climate change in the 21st century, Atmos. Environ., 43, 3520, 10.1016/j.atmosenv.2009.04.024
Brooker, 2006, Civil aircraft design priorities: air quality? climate change? noise?, Aeronaut. J., 110, 517, 10.1017/S0001924000001408
Parker, 2009, From blue skies to green skies: engine technology to reduce the climate-change impacts of aviation, Technol. Anal. Strateg. Manag., 21, 61, 10.1080/09537320802557301
Lee, 2010, Transport impacts on atmosphere and climate: Aviation, Atmos. Environ., 44, 4678, 10.1016/j.atmosenv.2009.06.005
Ribeiro, 2007
Wuebbles, 2007, Evaluating the impacts of aviation on climate change, EOS Trans. Am. Geophys. Union, 88, 157, 10.1029/2007EO140001
Arrowsmith, 2020
2021
Schäfer, 2019, Technological, economic and environmental prospects of all-electric aircraft, Nat. Energy, 4, 160, 10.1038/s41560-018-0294-x
Ansell, 2020, Electrified airplanes: A path to zero-emission air travel, IEEE Electrif. Mag., 8, 18, 10.1109/MELE.2020.2985482
Prandtl, 1924
Frediani, 2009, Best wing system: an exact solution of the Prandtl’s problem — in: Variational analysis and aerospace engineering: Mathematical challenges for aerospace design, 183
Abu Salem, 2021, A physics-based multidisciplinary approach for the preliminary design and performance analysis of a medium range aircraft with box-wing architecture, Aerospace, 8, 1, 10.3390/aerospace8100292
Sahoo, 2020, A review of concepts, benefits, and challenges for future electrical propulsion-based aircraft, Aerospace, 7, 1, 10.3390/aerospace7040044
Bottone, 2012
Wagner, 2013, Current research trends and prospects among the various materials and designs used in lithium-based batteries, J. Appl. Electrochem., 43, 481, 10.1007/s10800-013-0533-6
Thackeray, 2012, Electrical energy storage for transportation - Approaching the limits of, and going beyond, lithium-ion batteries, Energy Environ. Sci., 5, 7854, 10.1039/c2ee21892e
Armand, 2020, Lithium-ion batteries – Current state of the art and anticipated developments, J. Power Sources, 479, 1, 10.1016/j.jpowsour.2020.228708
Nitta, 2015, Li-ion battery materials: present and future, Mater. Today, 18, 252, 10.1016/j.mattod.2014.10.040
Liu, 2016, Understanding electrochemical potentials of cathode materials in rechargeable batteries, Mater. Today, 19, 109, 10.1016/j.mattod.2015.10.009
Xiao, 2020, Understanding and applying coulombic efficiency in lithium metal batteries, Nat. Energy, 5, 561, 10.1038/s41560-020-0648-z
Sauer, 2009, Batteries — charge–discharge curves, 443
P. Vratny, C. Gologan, C. Pornet, Battery Pack Modeling Methods for Universally-Electric Aircraft, in: Proceedings of 4th CEAS Air & Space Conference, 16–19 September, Linköping, Sweden, 2013.
Van den Bossche, 2006, SUBAT: An assessment of sustainable battery technology, J. Power Sources, 162, 913, 10.1016/j.jpowsour.2005.07.039
Xue, 2015, Lithium-ion batteries: Thermomechanics, performance, and design optimization, 1
Qanungo, 2009, 11
Löbberding, 2020, From cell to battery system in BEVs: Analysis of system packing efficiency and cell types, World Electr. Veh. J., 11, 1
Ghiji, 2020, A review of lithium-ion battery fire suppression, Energies, 13, 1, 10.3390/en13195117
Boaretto, 2021, Lithium solid-state batteries: State-of-the-art and challenges for materials, interfaces and processing, J. Power Sources, 502, 1, 10.1016/j.jpowsour.2021.229919
Janek, 2016, A solid future for battery development, Nat. Energy, 1, 1, 10.1038/nenergy.2016.141
Zhao, 2021, Roadmap of solid-state lithium-organic batteries toward 500 Wh kg−1, ACS Energy Lett., 6, 3287, 10.1021/acsenergylett.1c01368
Viswanathan, 2022, The challenges and opportunities of battery-powered flight, Nature, 601, 519, 10.1038/s41586-021-04139-1
Chen, 2021, A review of lithium-ion battery safety concerns: The issues, strategies, and testing standards, J. Energy Chem., 59, 83, 10.1016/j.jechem.2020.10.017
Chombo, 2020, A review of safety strategies of a Li-ion battery, J. Power Sources, 478, 1, 10.1016/j.jpowsour.2020.228649
Sripad, 2021, A review of safety considerations for batteries in aircraft with electric propulsion, MRS Bull., 46, 435, 10.1557/s43577-021-00097-1
Arora, 2018, Mechanical design and packaging of battery packs for electric vehicles, 175
Schröder, 2017, Comparatively assessing different shapes of lithium-ion battery cells, Procedia Manuf., 8, 104, 10.1016/j.promfg.2017.02.013
Dever, 2015
Dörfler, 2020, Recent progress and emerging application areas for lithium–sulfur battery technology, Energy Technol., 9, 1
Mikhaylik, 2016, Sion power’s licerion high energy batteries, 397
Winterkorn, 2022, Li-free anode development at quantumscape, 1733
Zhang, 2022
Xia, 2021, Thin lithium metal foil technology for advanced battery manufacturing, 362
Zhang, 2017, Li–S and Li–O2 batteries with high specific energy, 1
Gallagher, 2014, Quantifying the promise of lithium–air batteries for electric vehicles, Energy Environ. Sci., 7, 1555, 10.1039/c3ee43870h
R. Bugga, C. Krause, M. Smart, W. West, E. Brandon, Battery for electric aviation, in: NAATBatt Annual Meeting & Conference, 10–13 February, Pasadena, USA, 2020.
Zuo, 2017, Battery-supercapacitor hybrid devices: Recent progress and future prospects, Adv. Sci., 4, 1, 10.1002/advs.201600539
Li, 2016, Nitrogen-doped activated carbon for a high energy hybrid supercapacitor, Energy Environ. Sci., 9, 102, 10.1039/C5EE03149D
Dicks, 2018
Gierens, 2021, Theory of contrail formation for fuel cells, Aerospace, 8, 1, 10.3390/aerospace8060164
O’Hayre, 2016
J. Klier, M. Rattey, G. Kaiser, M. Klupsch, A. Kade, M. Schneider, R. Herzog, A new cryogenic high-pressure H2 test area: First results, in: 12th IIR International Conference, 11–14 September, Dresden, Germany, 2012.
Kadyk, 2018, Analysis and design of fuel cell systems for aviation, Energies, 11, 1, 10.3390/en11020375
Schröder, 2021, Optimal operating conditions of PEM fuel cells in commercial aircraft, Int. J. Hydrogen Energy, 46, 33218, 10.1016/j.ijhydene.2021.07.099
National Academies of Sciences, Engineering, and Medicine, 2016
Şahin, 2022, A comprehensive review on supercapacitor applications and developments, Energies, 15, 1, 10.3390/en15030674
2019, Technologies of energy storage systems, 17
A. Murray, P. Kettle, F. Moynihan, Advances in brushless motor control, in: Proceedings of the 1997 American Control Conference (ACC 1997), 4–6 June, Albuquerque, USA, 1997, http://dx.doi.org/10.1109/acc.1997.609647.
G.C.R. Sincero, J. Cros, P. Viarouge, Efficient simulation method for comparison of brush and brushless DC motors for light traction application, in: 13th European Conference on Power Electronics and Applications, 8–10 September, Barcelona, Spain, 2009, pp. 1–10.
Haran, 2017, High power density superconducting rotating machines—development status and technology roadmap, Supercond. Sci. Technol., 30, 1, 10.1088/1361-6668/aa833e
Bird, 2022, A review of electric aircraft drivetrain motor technology, IEEE Trans. Magn., 58, 1, 10.1109/TMAG.2021.3081719
Zhang, 2018, Large electric machines for aircraft electric propulsion, IET Electr. Power Appl., 12, 767, 10.1049/iet-epa.2017.0639
Vukosavic, 2012
Nøland, 2020, High-power machines and starter-generator topologies for more electric aircraft: A technology outlook, IEEE Access, 8, 130104, 10.1109/ACCESS.2020.3007791
Sirimanna, 2021, Comparison of electrified aircraft propulsion drive systems with different electric motor topologies, J. Propuls. Power, 37, 733, 10.2514/1.B38195
Rhebergen, 2015, Enhancement of electric motor thermal management through axial cooling methods: A materials approach
Canders, 2019, Cooling technologies for high power density electrical machines for aviation applications, Energies, 12, 4579, 10.3390/en12234579
Deisenroth, 2019, Thermal management of high-power density electric motors for electrification of aviation and beyond, Energies, 12, 1, 10.3390/en12193594
Masson, 2005, HTS motors in aircraft propulsion: design considerations, IEEE Trans. Appl. Supercond., 15, 2218, 10.1109/TASC.2005.849616
Masson, 2007, HTS machines as enabling technology for all-electric airborne vehicles, Supercond. Sci. Technol., 20, 748, 10.1088/0953-2048/20/8/005
Luongo, 2009, Next generation more-electric aircraft: A potential application for HTS superconductors, IEEE Trans. Appl. Supercond., 19, 1055, 10.1109/TASC.2009.2019021
Ganev, 2014, Selecting the best electric machines for electrical power-generation systems: High-performance solutions for aerospace more electric architectures, IEEE Electrif. Mag., 2, 13, 10.1109/MELE.2014.2364731
Sivasubramaniam, 2009, Development of a high speed HTS generator for airborne applications, IEEE Trans. Appl. Supercond., 19, 1656, 10.1109/TASC.2009.2017758
Dubensky, 2016, An outlook of the use of cryogenic electric machines onboard aircraft, IEEE Trans. Appl. Supercond., 26, 1, 10.1109/TASC.2016.2524656
Gieras, 2009, Superconducting electrical machines - state of the art, Prz. Elektrotech., 1
Kovalev, 2019, Multidisciplinary approach to the design of superconducting electrical machines, IOP Conf. Ser.: Mater. Sci. Eng., 581, 1, 10.1088/1757-899X/581/1/012012
Chow, 2023, High temperature superconducting rotating electrical machines: An overview, Energy Rep., 9, 1124, 10.1016/j.egyr.2022.11.173
Sirimanna, 2022, Electric propulsors for zero-emission aircraft: Partially superconducting machines, IEEE Electrif. Mag., 10, 43, 10.1109/MELE.2022.3165952
A. Seitz, O. Schmitz, A.T. Isikveren, Electrically powered propulsion: Comparison and contrast to gas turbines, in: Proceedings of 61st Deutscher Luft- und Raumfahrtkongress, 10–12 September, Berlin, Germany, 2012.
Jiang, 2023, A review on insulation challenges towards electrification of aircraft, High Volt., n/a, 1, 10.1049/hve2.12270
Arabul, 2021, Perspectives and development of electrical systems in more electric aircraft, Int. J. Aerosp. Eng., 2021, 1, 10.1155/2021/5519842
Benzaquen, 2021, Toward more electric powertrains in aircraft: Technical challenges and advancements, CES Trans. Electr. Mach. Syst., 5, 177, 10.30941/CESTEMS.2021.00022
Mohan, 2023, Systems integration considerations for hybrid-electric commuter aircraft: Case study for the DO-228
Bolam, 2020, A review of electrical motor topologies for aircraft propulsion
de Carvalho Pinheiro, 2022, In-wheel and on-board motors in BEV: lateral and vertical performance comparison
Moreno Bravo, 2021, Performance analysis of hybrid electric and distributed propulsion system applied on a light aircraft, Energy, 214, 1
Baerheim, 2023, Potential and limitations of battery-powered all-electric regional flights—A norwegian case study, IEEE Trans. Transp. Electrif., 9, 1809, 10.1109/TTE.2022.3200089
Ivanov, 2022, Electric machines with high specific power, Russ. Electr. Eng., 93, 621, 10.3103/S1068371222100054
Alvarez, 2022, Review of high power and high voltage electric motors for single-aisle regional aircraft, IEEE Access, 10, 112989, 10.1109/ACCESS.2022.3215692
Yoon, 2016, A high-speed, high-frequency, air-core PM machine for aircraft application
Yi, 2017, Multi-physics optimization for high-frequency air-core permanent-magnet motor of aircraft application
Yi, 2018, Self-pumped air-cooling design for a high-speed high-specific-power motor
Jansen, 2018, High efficiency megawatt motor conceptual design
Scheidler, 2018, Preliminary design of the superconducting rotor for NASA’s 1.4 MW high-efficiency electric machine
Tallerico, 2020, Electromagnetic redesign of NASA’s high efficiency megawatt motor
Tallerico, 2021, Design optimization studies of partially superconducting machines based on NASA’s high efficiency megawatt motor
Farrakhov, 2020, Novel modular design of gearless electric drive for propeller of an all-electric aircraft
Kozlova, 2021, Technical advances in aviation electrification: Enhancing strategic R&D investment analysis through simulation decomposition, Sustainability, 14, 1, 10.3390/su14010414
Silberhorn, 2020, Multidisciplinary investigation of partially turboelectric, boundary layer ingesting aircraft concepts CleanSky2 LPA WP1.6.1 special session
Swanke, 2019, Comparison of modular PM propulsion machines for high power density
Sethi, 2022, Enabling cryogenic hydrogen-based CO2-free air transport: Meeting the demands of zero carbon aviationn, IEEE Electrif. Mag., 10, 69, 10.1109/MELE.2022.3165955
Khandelwal, 2013, Hydrogen powered aircraft: The future of air transport, Prog. Aerosp. Sci., 60, 45, 10.1016/j.paerosci.2012.12.002
Baroutaji, 2019, Comprehensive investigation on hydrogen and fuel cell technology in the aviation and aerospace sectors, Renew. Sustain. Energy Rev., 106, 31, 10.1016/j.rser.2019.02.022
Gangoli Rao, 2020, Energy transition in aviation: The role of cryogenic fuels, Aerospace, 7, 1
Prewitz, 2020, Hydrogen as the fuel of the future in aircrafts – Challenges and opportunities, Int. J. Hydrogen Energy, 45, 25378, 10.1016/j.ijhydene.2020.06.238
Silberhorn, 2022, Climate impact reduction potentials of synthetic kerosene and green hydrogen powered mid-range aircraft concepts, Appl. Sci., 12, 1, 10.3390/app12125950
Buticchi, 2022, The more-electric aircraft and beyond, Proc. IEEE, 1
S. Kicin, F. Traub, S. Hartmann, E. Bianda, C. Bernhard, S. Skibin, F. Canales, A new concept of a high-current power module allowing paralleling of many SiC devices assembled exploiting conventional packaging technologies, in: 28th International Symposium on Power Semiconductor Devices and ICs (ISPSD), 12–16 June, Prague, Czech Republic, 2016, pp. 467–470, http://dx.doi.org/10.1109/ISPSD.2016.7520879.
Tolbert, 2002, Impact of SiC power electronic devices for hybrid electric vehicles
Wileman, 2021, A road map for reliable power electronics for more electric aircraft, Prog. Aerosp. Sci., 127, 1, 10.1016/j.paerosci.2021.100739
Han, 2014, Comprehensive efficiency, weight, and volume comparison of SiC- and Si-based bidirectional DC-DC converters for hybrid electric vehicles, IEEE Trans. Veh. Technol., 63, 3001, 10.1109/TVT.2014.2323193
Richard, 2023, AC electric powertrain without power electronics for future hybrid electric aircrafts: Architecture, design and stability analysis, Appl. Sci., 13, 672, 10.3390/app13010672
Barzkar, 2022, Components of electrical power systems in more and all-electric aircraft: A review, IEEE Trans. Transp. Electrif., 8, 4037, 10.1109/TTE.2022.3174362
Alves Eleodoro, 2022, Analysis of SiC and SiC-Cascode MOSFET in the design of power electronics converters for more electric aircrafts, Int. J. Power Electron. Drive Syst. (IJPEDS), 13, 1
Jansen, 2017, Overview of NASA electrified aircraft propulsion research for large subsonic transports
Wang, 2022, Power electronics: A critical enabler of future hydrogen–electric systems for aviation, IEEE Electrif. Mag., 10, 57, 10.1109/MELE.2022.3165954
Luo, 2022, High-density motor drive development for electric aircraft propulsion: Cryogenic and non-cryo solutions
Fard, 2022, Aircraft distributed electric propulsion technologies—A review, IEEE Trans. Transp. Electrif., 8, 4067, 10.1109/TTE.2022.3197332
Dorn-Gomba, 2020, Power electronic converters in electric aircraft: Current status, challenges, and emerging technologies, IEEE Trans. Transp. Electrif., 6, 1648, 10.1109/TTE.2020.3006045
Rahrovi, 2019, A review of the more electric aircraft power electronics
Ni, 2019, Electrical and electronic technologies in more-electric aircraft: A review, IEEE Access, 7, 76145, 10.1109/ACCESS.2019.2921622
Barzkar, 2020, Electric power systems in more and all electric aircraft: A review, IEEE Access, 8, 169314, 10.1109/ACCESS.2020.3024168
Bourdon, 2015, Review of power electronics opportunities to integrate in the more electrical aircraft
Cinar, 2020, A framework for electrified propulsion architecture and operation analysis, Aircr. Eng. Aerosp. Technol., 92, 675, 10.1108/AEAT-06-2019-0118
Gohardani, 2011, Challenges of future aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric commercial aircraft, Prog. Aerosp. Sci., 47, 369, 10.1016/j.paerosci.2010.09.001
Isikveren, 2015, Distributed propulsion and ultra-high by-pass rotor study at aircraft level, Aeronaut. J., 119, 1327, 10.1017/S0001924000011295
Wick, 2015, Integrated aerodynamic benefits of distributed propulsion
Isikveren, 2014, Pre-design strategies and sizing techniques for dual-energy aircraft, Aircr. Eng. Aerosp. Technol., 86, 525, 10.1108/AEAT-08-2014-0122
Palaia, 2022
Zaretsky, 1983
Seitz, 2018, Conceptual study of a mechanically integrated parallel hybrid electric turbofan, Proc. Inst. Mech. Eng. G, 232, 2688, 10.1177/0954410018790141
Schmitz, 2013, Unified applicable propulsion system performance metrics, J. Eng. Gas Turbines Power, 135, 1, 10.1115/1.4025066
N. Madavan, A NASA Perspective on Electric Propulsion Technologies for Commercial Aviation, in: International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and the International Transportation Electrification Conference (ESARS-ITEC), 4 November, Toulouse, France, 2016.
Martulli, 2020, A thick-walled sheet moulding compound automotive component: Manufacturing and performance, Composites A, 128, 1, 10.1016/j.compositesa.2019.105688
M. Cardone, B. Gargiulo, E. Fornaro, Development of a flexible test bench for a Hybrid Electric Propulsion System, in: IEEE International Workshop on Metrology for Automotive (MetroAutomotive), 1–2 July, Virtual event, 2021, pp. 221–225, http://dx.doi.org/10.1109/MetroAutomotive50197.2021.9502723.
M.A. Rendon, C.D. Sanchez, J. Gallo, J.F. Garcia, N. Xiong, Using differential evolution techniques for management of a hybrid-electric propulsion system, in: Brazilian Conference on Automation BCA20, 23–26 November, Porto Alegre, Brasil, 2020.
Finger, 2020, Initial sizing methodology for hybrid-electric general aviation aircraft, J. Aircr., 57, 245, 10.2514/1.C035428
Geiß, 2017, Sizing of the energy storage system of hybrid-electric aircraft in general aviation, CEAS Aeronaut. J., 8, 53, 10.1007/s13272-016-0220-5
Riboldi, 2016, An integrated approach to the preliminary weight sizing of small electric aircraft, Aerosp. Sci. Technol., 58, 134, 10.1016/j.ast.2016.07.014
Hospodka, 2020, Assessment of all-electric general aviation aircraft, Energies, 13, 1, 10.3390/en13236206
Nicolosi, 2015, Design and aerodynamic analysis of a twin-engine commuter aircraft, Aerosp. Sci. Technol., 40, 1, 10.1016/j.ast.2014.10.008
Nicolosi, 2016, Commuter aircraft aerodynamic characteristics through wind tunnel tests, Aircr. Eng. Aerosp. Technol., 88, 523, 10.1108/AEAT-01-2015-0008
Salucci, 2021, Capturing the demand for an electric-powered short-haul air transportation network
Orefice, 2022, Design of hybrid-electric small air transports, IOP Conf. Ser.: Mater. Sci. Eng., 1226, 1, 10.1088/1757-899X/1226/1/012075
Orefice, 2020, Aircraft conceptual design of commuter aircraft including distributed electric propulsion
A. Rolando, F. Salucci, L. Trainelli, C.E. Riboldi, Y.M. Khan, On the Design of an Electric-Powered Micro-Feeder Aircraft, in: 1st Aerospace Europe Conference (AEC 2020), 25–28 February, Bordeaux, France, 2020.
Isikveren, 2018, Pre-design of a commuter transport utilising Voltaic-Joule/Brayton motive power systems, Aeronaut. J., 122, 205, 10.1017/aer.2017.126
P. Wassink, G. Atanasov, C. Hesse, B. Fröhler, Conceptual Design of Silent Electric Commuter Aircraft, in: 32nd Congress of the International Council of the Aeronautical Sciences (ICAS 2021), 6–10 September, Shanghai, China, 2021.
Ciliberti, 2022, The enabling technologies for a quasi-zero emissions commuter aircraft, Aerospace, 9, 1, 10.3390/aerospace9060319
Donateo, 2022, A methodology for the comparative analysis of hybrid electric and all-electric power systems for urban air mobility, Energies, 15, 1, 10.3390/en15020638
Bacchini, 2019, Electric VTOL configurations comparison, Aerospace, 6, 1, 10.3390/aerospace6030026
Palaia, 2021, A conceptual design methodology for e-VTOL aircraft for urban air mobility, Appl. Sci., 11, 1, 10.3390/app112210815
D.F. Finger, F. Götten, C. Braun, C. Bil, Initial sizing for a family of hybrid-electric VTOL general aviation aircraft, in: Deutscher Luft- und Raumfahrtkongress, 4–6 September, Friedrichshafen, Germany, 2018, http://dx.doi.org/10.25967/480102.
Rajendran, 2020, Air taxi service for urban mobility: A critical review of recent developments, future challenges, and opportunities, Transp. Res. E, 143, 1, 10.1016/j.tre.2020.102090
Akash, 2022, Design and analysis of VTOL operated intercity electrical vehicle for urban air mobility, Electronics, 11, 1
Pornet, 2015, Methodology for sizing and performance assessment of hybrid energy aircraft, J. Aircr., 52, 341, 10.2514/1.C032716
Ang, 2019, Performance analysis of an electrically assisted propulsion system for a short-range civil aircraft, Proc. Inst. Mech. Eng. G, 233, 1490, 10.1177/0954410017754146
K. Abu Salem, V. Cipolla, G. Palaia, V. Binante, D. Zanetti, Conceptual study of hybrid-electric box-wing aircraft towards the reduction of aviation effects on local air quality and climate change, in: 33rd Congress of the International Council of the Aeronautical Sciences, 4–9 September, Stockholm, Sweeden, 2022.
Cipolla, 2020, Preliminary design and performance analysis of a box-wing transport aircraft
Abu Salem, 2018, PARSIFAL project: a breakthrough innovation in air transport, Aerotec. Missili Spaz., 97, 40, 10.1007/BF03404764
ICAO, 2017
Pornet, 2015, Conceptual design of hybrid-electric transport aircraft, Prog. Aerosp. Sci., 79, 114, 10.1016/j.paerosci.2015.09.002
ICAO, 2022
Sgueglia, 2020, Multidisciplinary design optimization framework with coupled derivative computation for hybrid aircraft, J. Aircr., 57, 715, 10.2514/1.C035509
A. Ko, J.A. Schetz, W.H. Mason, Assessment of the potential advantages of distributed-propulsion for aircraft, in: XVI International Symposium on Air Breathing Engines (ISABE), August 31 - September 5, Cleveland, USA, 2003, paper ISABE-2003-1094.
Schmollgruber, 2019, Multidisciplinary exploration of DRAGON: an ONERA hybrid electric distributed propulsion concept
Risse, 2015, Central reference aircraft data system (CeRAS) for research community, CEAS Aeronaut. J., 7, 121, 10.1007/s13272-015-0177-9
Gnadt, 2019, Technical and environmental assessment of all-electric 180-passenger commercial aircraft, Prog. Aerosp. Sci., 105, 1, 10.1016/j.paerosci.2018.11.002
Rompokos, 2021, Synergistic technology combinations for future commercial aircraft using liquid hydrogen, J. Eng. Gas Turbines Power, 143, 1, 10.1115/1.4049694
Chiaramonti, 2019, Sustainable aviation fuels: the challenge of decarbonization, Energy Procedia, 158, 1202, 10.1016/j.egypro.2019.01.308
Ng, 2021, Global biorenewable development strategies for sustainable aviation fuel production, Renew. Sustain. Energy Rev., 150, 1, 10.1016/j.rser.2021.111502
Zhang, 2020, Recent trends, opportunities and challenges of sustainable aviation fuel, 85
Eisenhut, 2021, Aircraft requirements for sustainable regional aviation, Aerospace, 8, 1, 10.3390/aerospace8030061
Prapotnik Brdnik, 2019, Market and technological perspectives for the new generation of regional passenger aircraft, Energies, 12, 1, 10.3390/en12101864
de Vries, 2019, Preliminary sizing method for hybrid-electric distributed-propulsion aircraft, J. Aircr., 56, 2172, 10.2514/1.C035388
Voskuijl, 2017, Analysis and design of hybrid electric regional turboprop aircraft, CEAS Aeronaut. J., 9, 15, 10.1007/s13272-017-0272-1
Gesell, 2019, System analysis of turbo-electric and hybrid-electric propulsion systems on a regional aircraft, Aeronaut. J., 123, 1602, 10.1017/aer.2019.61
Finger, 2020, Comparative assessment of parallel-hybrid-electric propulsion systems for four different aircraft, J. Aircr., 57, 843, 10.2514/1.C035897
Hoelzen, 2018, Conceptual design of operation strategies for hybrid electric aircraft, Energies, 11, 1, 10.3390/en11010217
Hainsch, 2020, European green deal: Using ambitious climate targets and renewable energy to climb out of the economic crisis, DIW Wkly. Rep., 10, 303
Brueckner, 2010, Airline emission charges: Effects on airfares, service quality, and aircraft design, Transp. Res. B, 44, 960, 10.1016/j.trb.2010.02.006
McConnachie, 2013, The impact of fuel price on airline fuel efficiency and operations
Antcliff, 2016, Mission analysis and aircraft sizing of a hybrid-electric regional aircraft
S. Stückl, J. van Toor, H. Lobentanzer, VOLTAIR - The All Electric Propulsion Concept Platform - A Vision for Atmospheric Friendly Flight, in: Proceedings of the 28th International Congress of the Aeronautical Sciences (ICAS), 23–28 September, Brisbane, Australia, 2012.
Karpuk, 2021, Influence of novel airframe technologies on the feasibility of fully-electric regional aviation, Aerospace, 8, 1, 10.3390/aerospace8060163
Yarygina, 2012, Development of the weight formula for a folding wing, Russ. Aeronaut., 55, 120, 10.3103/S106879981202002X
D. Scholz, Limits to Principles of Electric Flight, in: Proceedings of the Deutscher Luft- und Raumfahrtkongress, 30 September–2 October, Darmstadt, Germany, 2019, http://dx.doi.org/10.5281/ZENODO.4072283.
Zaporozhets, 2020, Trends on current and forecasted aircraft hybrid electric architectures and their impact on environment, Energy, 211, 1, 10.1016/j.energy.2020.118814
Pornet, 2014, Integrated fuel-battery hybrid for a narrow-body sized transport aircraft, Aircr. Eng. Aerosp. Technol., 86, 568, 10.1108/AEAT-05-2014-0062
Arnaldo Valdés, 2021, How much can carbon taxes contribute to aviation decarbonization by 2050, Sustainability, 13, 1
Bravo-Mosquera, 2022, Unconventional aircraft for civil aviation: A review of concepts and design methodologies, Prog. Aerosp. Sci., 131, 1, 10.1016/j.paerosci.2022.100813
McDonald, 2021, Future aircraft concepts and design methods, Aeronaut. J., 126, 92, 10.1017/aer.2021.110
Cavallaro, 2016, Challenges, ideas, and innovations of joined-wing configurations: A concept from the past, an opportunity for the future, Prog. Aerosp. Sci., 87, 1, 10.1016/j.paerosci.2016.07.002
Abbas, 2013, Aerodynamic technologies to improve aircraft performance, Aerosp. Sci. Technol., 28, 100, 10.1016/j.ast.2012.10.008
Green, 2006, Civil aviation and the environment — the next frontier for the aerodynamicist, Aeronaut. J., 110, 469, 10.1017/S0001924000001378
Graham, 2014, The potential of future aircraft technology for noise and pollutant emissions reduction, Transp. Policy, 34, 36, 10.1016/j.tranpol.2014.02.017
Gagnon, 2014, High-fidelity aerodynamic shape optimization of unconventional aircraft through axial deformation
M. Iwanizki, S. Wöhler, B. Fröhler, T. Zill, M. Méheut, S. Defoort, M. Carini, J. Gauvrit-Ledogar, R. Liaboeuf, A. Tremolet, B. Paluch, S. Kanellopoulos, Conceptual design studies of unconventional configurations, in: Aerospace Europe Conference (AEC2020), 25–28 February, Bordeaux, France, 2020.
Frediani, 2012, The PrandtlPlane configuration: Overview on possible applications to civil aviation — in: Variational analysis and aerospace engineering: Mathematical challenges for aerospace design, 179
Frediani, 2005, The Prandtl wing
Bravo-Mosquera, 2022, Design, aerodynamic analysis and optimization of a next-generation commercial airliner, J. Braz. Soc. Mech. Sci. Eng., 44, 1, 10.1007/s40430-022-03924-x
Demasi, 2014, Invariant formulation for the minimum induced drag conditions of nonplanar wing systems, AIAA J., 52, 2223, 10.2514/1.J052837
Cipolla, 2018, Conceptual design of a box-wing aircraft for the air transport of the future
Bishop, 2012
Pornet, 2014, Cost-based flight technique optimization for hybrid energy aircraft, Aircr. Eng. Aerosp. Technol., 86, 591, 10.1108/AEAT-05-2014-0075
Tasca, 2021, Innovative box-wing aircraft: Emissions and climate change, Sustainability, 13, 1, 10.3390/su13063282
Proesmans, 2022, Airplane design optimization for minimal global warming impact, J. Aircr., 59, 1363, 10.2514/1.C036529
Hudda, 2020, Impacts of aviation emissions on near-airport residential air quality, Environ. Sci. Technol., 54, 8580, 10.1021/acs.est.0c01859
Yang, 2018, Characterization of aircraft emissions and air quality impacts of an international airport, J. Environ. Sci., 72, 198, 10.1016/j.jes.2018.01.007
Zhu, 2011, Aircraft emissions and local air quality impacts from takeoff activities at a large international airport, Atmos. Environ., 45, 6526, 10.1016/j.atmosenv.2011.08.062
Simonetti, 2015, Air quality impact of a middle size airport within an urban context through EDMS simulation, Transp. Res. D, 40, 144, 10.1016/j.trd.2015.07.008
Stettler, 2011, Air quality and public health impacts of UK airports. Part I: Emissions, Atmos. Environ., 45, 5415, 10.1016/j.atmosenv.2011.07.012
Brelje, 2019, Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches, Prog. Aerosp. Sci., 104, 1, 10.1016/j.paerosci.2018.06.004
Kougias, 2021, The role of photovoltaics for the European Green Deal and the recovery plan, Renew. Sustain. Energy Rev., 144, 1, 10.1016/j.rser.2021.111017
Palaia, 2021, THEA-CODE: a design tool for the conceptual design of hybrid-electric aircraft with conventional or unconventional airframe configurations, Mech. Ind., 22, 19, 10.1051/meca/2021012
G. Palaia, K. Abu Salem, V. Cipolla, D. Zanetti, V. Binante, Preliminary comparison of box-wing and tube-and-wing hybrid-electric regional aircraft, in: AIDAA XXVI International Congress, 31 August - 3 September, Pisa, Italy, 2021.
Abu Salem, 2021, Tools and methodologies for box-wing aircraft conceptual aerodynamic design and aeromechanic analysis, Mech. Ind., 22, 1
Rizzo, 2009, Application of optimisation algorithms to aircraft aerodynamics — in: Variational analysis and aerospace engineering: Mathematical challenges for aerospace design, 419
Rizzo, 2009
Cappelli, 2016, Aerodynamic optimization of a large PrandtlPlane configuration, Aerotec. Missili Spaz., 95, 163, 10.1007/BF03404725
Drela, 2017
Raymer, 2018
Drela, 2001
Svoboda, 2000, Turbofan engine database as a preliminary design tool, Aircr. Des., 3, 17, 10.1016/S1369-8869(99)00021-X
Kuz’michev, 2018, Comparative analysis of mathematical models for turbofan engine weight estimation, MATEC Web Conf., 220, 1, 10.1051/matecconf/201822003012
Wells, 2017
Cipolla, 2021, A DoE-based approach for the implementation of structural surrogate models in the early stage design of box-wing aircraft, Aerosp. Sci. Technol., 117, 1, 10.1016/j.ast.2021.106968
Palaia, 2023, A DoE - based scalable approach for the preliminary structural design of Box-Wing aircraft from regional to medium range categories
Gary Wang, 2006, Review of metamodeling techniques in support of engineering design optimization, J. Mech. Des., 129, 370, 10.1115/1.2429697
Simpson, 2001, Metamodels for computer-based engineering design: Survey and recommendations, Eng. Comput., 17, 129, 10.1007/PL00007198
Rizzo, 2019
Picchi Scardaoni, 2017, WAGNER: a new code for parametrical structural study of fuselages of civil transport aircraft, Aerotec. Missili Spaz., 96, 136, 10.1007/BF03404748
Dassault Systèmes Simulia Corp, ABAQUS User Manual.
Torenbeek, 1992
Riboldi, 2019, Energy-optimal off-design power management for hybrid-electric aircraft, Aerosp. Sci. Technol., 95, 1, 10.1016/j.ast.2019.105507
Ruijgrok, 2009
Y. Mikhaylik, I. Kovalev, 650 Wh/kg, 1400 Wh/L Rechargeable Batteries for New Era of Electrified Mobility, in: NASA Aerospace Battery Workshop, 14–16 November, Huntsville, USA, 2018.
Anonymous, 2021
Abu Salem, 2021
Palaia, 2023, Mission performance analysis of hybrid-electric regional aircraft, Aerospace, 10, 1, 10.3390/aerospace10030246
Freeman, 2014, Challenges and opportunities for electric aircraft thermal management, Aircr. Eng. Aerosp. Technol., 86, 519, 10.1108/AEAT-04-2014-0042
Courtin, 2018, Safety considerations in emerging electric aircraft architectures
Yildiz, 2022, Initial airworthiness requirements for aircraft electric propulsion, Aircr. Eng. Aerosp. Technol., 94, 1357, 10.1108/AEAT-08-2021-0238
Yetik, 2021, Thermal management system with nanofluids for hybrid electric aircraft battery, Int. J. Energy Res., 45, 8919, 10.1002/er.6425
Kellermann, 2022, Design of a battery cooling system for hybrid electric aircraft, J. Propuls. Power, 38, 736, 10.2514/1.B38695
Riboldi, 2020, Predicting the effect of electric and hybrid-electric aviation on acoustic pollution, Noise Mapp., 7, 35, 10.1515/noise-2020-0004
Synodinos, 2018, Preliminary noise assessment of aircraft with distributed electric propulsion
Salucci, 2021, A noise estimation procedure for electric and hybrid-electric aircraft
Pinheiro Melo, 2020, Sustainability assessment and engineering of emerging aircraft technologies—Challenges, methods and tools, Sustainability, 12, 1, 10.3390/su12145663
Scholz, 2021, Environmental life cycle assessment and operating cost analysis of a conceptual battery hybrid-electric transport aircraft, CEAS Aeronaut. J., 13, 215, 10.1007/s13272-021-00556-0
Ribeiro, 2020, Environmental assessment of hybrid-electric propulsion in conceptual aircraft design, J. Clean. Prod., 247, 10.1016/j.jclepro.2019.119477
Barke, 2022, Comparison of conventional and electric passenger aircraft for short-haul flights – A life cycle sustainability assessment, Procedia CIRP, 105, 464, 10.1016/j.procir.2022.02.077
Barke, 2021, Life cycle sustainability assessment of potential battery systems for electric aircraft, Procedia CIRP, 98, 660, 10.1016/j.procir.2021.01.171
Salucci, 2021, Sizing of airport recharging infrastructures in support to a hybrid-electric fleet
Doctor, 2022, Modelling the effect of electric aircraft on airport operations and infrastructure, Technol. Forecast. Soc. Change, 177, 1, 10.1016/j.techfore.2022.121553
Trainelli, 2021, Optimal sizing and operation of airport infrastructures in support of electric-powered aviation, Aerospace, 8, 1, 10.3390/aerospace8020040