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Energy Sources, Part A: Recovery, Utilization, and Environmental Effects Volume 45, 2023 - Issue 1
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Research Article

Conceptual design analysis for a lightweight aircraft with a fuel cell hybrid propulsion system

Hüseyin Turan Arata Faculty of Engineering and Natural Sciences, Department of Mechatronics Engineering, Iskenderun Campus, İskenderun Technical University, Hatay, TurkeyCorrespondence[email protected]
ORCID Iconhttps://orcid.org/0000-0002-9269-4075View further author information
ORCID Icon,
Meryem Gizem Sürerb Faculty of Engineering and Natural Sciences, Department of Mechanical Engineering, Iskenderun Campus, İskenderun Technical University, Hatay, TurkeyView further author information
,
Semir Gökpinarb Faculty of Engineering and Natural Sciences, Department of Mechanical Engineering, Iskenderun Campus, İskenderun Technical University, Hatay, TurkeyView further author information
&
Kadir Aydinc Faculty of Engineering, Department of Mechanical Engineering, Çukurova University, Adana, TURKEYView further author information
Pages 46-60 | Received 29 Jan 2020, Accepted 20 May 2020, Published online: 10 Jun 2020

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Hasan Çınar, Süleyman Tunçel, Ilyas Kandemir & Tuba Gözel. (2023) Conceptual design and optimal sizing of a small unmanned aerial vehicle with fuel cell and battery-powered hybrid propulsion system by meta-heuristic algorithms based on energy consumption. Energy Sources, Part A: Recovery, Utilization, and Environmental Effects 45:1, pages 140-159.
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A'rasy Fahruddin, Djatmiko Ichsani, Fadlilatul Taufany, Budi Utomo Kukuh Widodo & Wawan Aries Widodo. (2022) Improved performance of polymer electrolyte membrane fuel cell using leaf-baffle flow field design. International Journal of Ambient Energy 43:1, pages 4782-4788.
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Xucheng Chang, Bing Kong & Farid Gholizadeh. (2022) Assessment and comparison of the operation of an unmanned aerial vehicle’s propulsion system based on the different fuel cells. Energy Sources, Part A: Recovery, Utilization, and Environmental Effects 44:2, pages 3294-3312.
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Articles from other publishers (10)

Yong Wang, Jiatong Du, Qijun Zhao & Haibo Zhang. (2023) Optimization Design and Analysis of Power Management for Serial Hybrid-Electric Propulsion System Under Aircraft/Engine Integrated Framework. International Journal of Aeronautical and Space Sciences.
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Gubran A. Q. Abdulrahman & Naef A. A. Qasem. (2023) Optimizing Endurance and Power Consumption of Fixed-Wing Unmanned Aerial Vehicles Powered by Proton-Exchange Membrane Fuel Cells. Arabian Journal for Science and Engineering.
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Eralp Sener, Isil Yazar, Gurhan Ertasgin & Hasan Yamik. (2023) Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario. International Journal of Turbo & Jet-Engines 40:2, pages 147-157.
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Karthik Kumar, Meeta Sharma & Anoop Kumar Shukla. 2023. Recent Advances in Mechanical Engineering. Recent Advances in Mechanical Engineering 249 262 .
Enes Gunaltili, Selcuk Ekici, Mustafa Zeki Yilmazoglu & Tahir Hikmet Karakoc. 2023. Emerging Trends in Electric Aviation. Emerging Trends in Electric Aviation 1 7 .
Medhat A. Nemitallah, MD Azazul Haque, Muzafar Hussain, Ahmed Abdelhafez & Mohamed A. Habib. (2022) Stratified and Hydrogen Combustion Techniques for Higher Turndown and Lower Emissions in Gas Turbines. Journal of Energy Resources Technology 144:2.
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Seunghun Shin, Yunkyeong Kim, Joon-Hyung Jin & Jihoon Jung. (2021) Heat-Induced Dry Hydrolysis of Sodium Borohydride/Oxalic Acid Dihydrate Composite for Hydrogen Production. ACS Omega 7:1, pages 979-986.
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Mohammed Amine Chetouane, Belkhir Negrou, Mohamed Becherif, Noureddine Settou, Abdessalem Bouferrouk & Mohamad Ramadan. (2021) Thermal Control for Electric Vehicle Based on the Multistack Fuel Cells. Energy Technology 9:9.
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Ana Lidia d. CastroPedro T. LacavaCarlos Henrique B. Mourão. (2021) Feasibility of Using Fuel Cell in a Small Aircraft. Feasibility of Using Fuel Cell in a Small Aircraft.
Eralp Sener, Isil Yazar, Gurhan Ertasgin & Hasan Yamik. (2020) Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario. International Journal of Turbo & Jet-Engines 0:0.
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