Skip to main content
Have a personal or library account? Click to login
Design and Performance Analysis of a Propeller for a Hybrid Turbo-Electric Propulsion System of a Regional Aircraft Cover

Design and Performance Analysis of a Propeller for a Hybrid Turbo-Electric Propulsion System of a Regional Aircraft

Open Access
|Jun 2026

References

  1. ACARE. ACARE vision. Advisory Council for Aviation Research and Innovation in Europe. Available from: https://www.acare4europe.org/acare-vision [cited 2025 Jun 1].
  2. Loginov V, Pushylin O, Tsaglov O. Review and analysis of integration properties of an aircraft with a hybrid power plant. In: Karakoc TH, Zaporozhets O, Dalkiran A, Ercan AH, editors. The future of electric aviation and artificial intelligence: ISEAS-ISUDEF 2023. Sustainable Aviation. Cham: Springer; 2025. https://doi.org/10.1007/978-3-031-62094-2_9
  3. Palaia G, Abu Salem K, Quarta AA. Parametric analysis for hybrid-electric regional aircraft conceptual design and development. Appl Sci. 2023; 13 (19): 11113. https://doi.org/10.3390/app131911113
  4. Thauvin J, Barraud G, Budinger M, Leray D, Roboam X, Sareni B. Hybrid regional aircraft: a comparative review of new potentials enabled by electric power. In: 52nd AIAA/SAE/ASEE Joint Propulsion Conference; 2016 Jul 25-27; Salt Lake City (UT). Reston (VA): AIAA; 2016. AIAA 2016-4612. https://doi.org/10.2514/6.2016-4612
  5. Alves P, Silvestre M, Gamboa P. Aircraft propellers — Is there a future? Energies. 2020;13(16):4157. https://doi.org/10.3390/en13164157
  6. Cardone LM, Petrone G, De Rosa S, Franco F, Greco CS. Review of the recent developments about the hybrid propelled aircraft. Aerotec Missili Spaz. 2024;103(1):17–37. https://doi.org/10.1007/s42496-023-00173-6
  7. Recoskie S, Fahim A, Gueaieb W, Lanteigne E. Experimental testing of a hybrid power plant for a dirigible UAV. J Intell Robot Syst. 2013;69(1-4):69–81. https://doi.org/10.1007/s10846-012-9764-8
  8. Hazeri M, Moradkhani M, Rashid Jafari J, Asadi D. Innovative synergies in aircraft propulsion: the concept of hybrid power systems with contra-rotating propellers. In: Proceedings of the ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition. Volume 1: Aircraft Engine; 2024 Jun 24-28; London, United Kingdom. New York (NY): ASME; 2024. p. V001T01A008. https://doi.org/10.1115/GT2024-121815
  9. Antcliff KR, Guynn MD, Marien T, Wells DP, Schneider SJ, Tong MJ. Mission analysis and aircraft sizing of a hybrid-electric regional aircraft. In: 54th AIAA Aerospace Sciences Meeting; 2016 Jan 4-8; San Diego (CA). Reston (VA): AIAA; 2016. AIAA 2016-1028. https://doi.org/10.2514/6.2016-1028
  10. Schouten T, Hoogreef M, Vos R. Effect of propeller installation on performance indicators of regional turboprop aircraft. In: AIAA Scitech 2019 Forum; 2019 Jan 7-11; San Diego (CA). Reston (VA): AIAA; 2019. AIAA 2019-1306. https://doi.org/10.2514/6.2019-1306
  11. Hoyos JD, Jiménez JH, Echavarría C, Alvarado JP, Urrea G. Aircraft propeller design through constrained aero-structural particle swarm optimization. Aerospace. 2022;9(3):153. https://doi.org/10.3390/aerospace9030153
  12. Ciliberti D, Nicolosi F. Design, analysis, and testing of a scaled propeller for an innovative regional turboprop aircraft. Aerospace. 2022;9(5):264. https://doi.org/10.3390/aerospace9050264
  13. Wang K, Zhou Z, Fan Z, Guo J. Aerodynamic design of tractor propeller for high-performance distributed electric propulsion. Chin J Aeronaut. 2021;34(10):20–35. https://doi.org/10.1016/j.cja.2021.01.008
  14. Huang Z, Yao H, Sjögren O, Lundbladh A, Davidson L. Aeroacoustic analysis of aerodynamically optimized joined-blade propeller for future electric aircraft at cruise and take-off. Aerosp Sci Technol. 2020;107:106336. https://doi.org/10.1016/j.ast.2020.106336
  15. Lück S, Göing J, Wittmann T, Kirsch B, Benjamin L, Friedrichs J. Propeller design and performance evaluation with partially prescribed velocity distribution. In: Proceedings of the Global Power and Propulsion Society Technical Conference; 2021. https://doi.org/10.33737/gpps21-tc-328
  16. Mel’nikov AP, Svechnikov VV. Teoriya i raschet lopastey vinta. Chast’ 1 [Theory and calculation of propeller blades. Part 1]. Leningrad: LKVVIA; 1947. (in Russian).
  17. Adkins CN, Liebeck RH. Design of optimum propellers. J Propuls Power. 1994;10(5):676–82. https://doi.org/10.2514/3.23779
  18. McGhee RJ, Beasley WD. Low-speed aerodynamic characteristics of a 17-percent-thick airfoil section designed for general aviation applications. NASA TN D-7428. Hampton (VA): NASA Langley Research Center; 1973.
  19. Langtry RB. A correlation-based transition model using local variables for unstructured parallelized CFD code [doctoral thesis]. Stuttgart: University of Stuttgart; 2006. 104 p. https://doi.org/10.18419/opus-1705
  20. Setlak L, Kowalik R, Lusiak T. Practical use of composite materials used in military aircraft. Materials. 2021;14(17):4812. https://doi.org/10.3390/ma14174812
Language: English
Page range: 38 - 52
Submitted on: Aug 21, 2025
Accepted on: Apr 16, 2026
Published on: Jun 17, 2026
In partnership with: Paradigm Publishing Services

© 2026 Anton Koshel, Oleksandr Yelans`ky, Vasyl Loginov, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.