FARKLI YÖNDEN GELEN RÜZGÂRIN İHA MOTOR PERVANESİ ÜZERİNDEKİ ETKİSİ: BİR DERLEME

Şükrü Eldek; Selim Tangöz

doi:10.17780/ksujes.1687992

EN TR

EFFECT OF WIND COMING FROM DIFFERENT DIRECTIONS ON UAV ENGINE PROPELLER: A REVIEW

Abstract

This review study examines research focused on the performance of unmanned aerial vehicle (UAV) propellers under varying wind directions. The study provides a detailed evaluation of analyses conducted through both experimental and numerical methods. It has been determined that changes in wind direction significantly impact the flight stability and efficiency of UAVs, with crosswind conditions in particular causing asymmetric loading on the propellers, leading to reduced efficiency and increased energy consumption. The reviewed studies demonstrate that propellers with different rotational speeds and pitch angles have been analyzed practically through wind tunnel testing and digitally through advanced simulation techniques such as Computational Fluid Dynamics (CFD). The results reveal that variations in wind direction and speed lead to significant differences in critical performance parameters such as thrust, torque, and overall efficiency. Moreover, the study offers recommendations for optimizing propeller designs to better adapt to changing atmospheric conditions. These findings provide valuable guidance for achieving more stable and efficient flight performance in future UAV designs.

Keywords

FARKLI YÖNDEN GELEN RÜZGÂRIN İHA MOTOR PERVANESİ ÜZERİNDEKİ ETKİSİ: BİR DERLEME

Öz

Bu derleme çalışması, insansız hava araçları (İHA) pervanelerinin farklı rüzgâr yönleri altında gösterdiği performansı inceleyen araştırmaları kapsamaktadır. Çalışmada, deneysel ve sayısal yöntemlerle yapılan analizler detaylı bir şekilde değerlendirilmiştir. Rüzgâr yönündeki değişimlerin İHA’ların uçuş stabilitesi ve verimliliği üzerinde belirgin etkiler yarattığı, özellikle çapraz rüzgâr koşullarında pervanelerde asimetrik yüklenmelere bağlı olarak verim düşüşü ve enerji tüketiminde artış gözlemlendiği belirlenmiştir. İncelenen çalışmalar, farklı devir hızları ve hatve açılarına sahip pervanelerin rüzgâr tüneli testleriyle pratikte, CFD gibi simülasyon teknikleriyle dijital ortamda analiz edildiğini göstermektedir. Sonuçlar, rüzgâr yönü ve hızındaki değişimlerin itiş, tork ve genel verimlilik gibi kritik performans parametrelerinde önemli farklılıklara yol açtığını ortaya koymuştur. Çalışma ayrıca, değişken hava koşullarına uyum sağlayacak şekilde pervane tasarımında yapılabilecek optimizasyonlara dair öneriler sunmaktadır. Bu bulgular, gelecekteki İHA tasarımlarında daha stabil ve verimli uçuş performansı sağlanması açısından önemli bir rehber niteliğindedir.

Anahtar Kelimeler

Kaynakça

Adkins, C.N. & Liebeck, R.H. (1981). Design of optimum propellers. *Journal of Propulsion and Power*, 1(3), 193-201. https://doi.org/10.2514/3.19779
Baker, F.R.L. & Smith, K.L. (2021). Aerodynamic performance of propellers at low Reynolds numbers. *Journal of Aircraft Engineering*, 58(3), 345-359. https://doi.org/10.1016/j.jaeng.2021.03.005
Becker, S., Lauenroth, A., & Rohardt, C.H. (2022). Propeller performance testing in the Cryogenic Wind Tunnel Cologne (DNW-KKK). *AIAA Aviation Forum*, Chicago, USA. https://doi.org/10.2514/6.2022-3456
Biermann, D. & Gray, W.H. (1941). Wind-tunnel tests of eight-blade single and dual-rotating pusher propellers in the tractor position. *NACA Advanced Research Report*, ARR-1005.
Bogdanski, J., Smith, R. & Johnson, M. (2015). The influence of blade pitch and rotational speed on propeller performance in aviation. *Journal of Aerospace Engineering*, 29(4), 567-580. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000543
Brandt, J.B. & Selig, M.S. (2011). Propeller performance data at low Reynolds numbers. *Journal of Aircraft*, 48(2), 700-709. https://doi.org/10.2514/1.C031114
Cai, J. & Gunasekaran, S. (2023). Frequency response of RC propellers to streamwise gusts in forward flight. *Wind*, 3(2), 253-272. https://doi.org/10.3390/wind3020015
Carroll, J. & Marcum, D. (2013). Comparison of a blade element momentum model to 3D CFD simulations for small scale propellers. *SAE International Journal of Aerospace*, 6(2), 721-728. https://doi.org/10.4271/2013-01-2185

Cerny, M. & Breitsamter, C. (2020). A comparison of isolated and ducted fixed-pitch propellers under non-axial inflow conditions. *Aerospace*, 7(8), 112. https://doi.org/10.3390/aerospace7080112
Chae, T., Kim, Y. & Park, D. (2018). Effects of blade design parameters on propeller performance. *Korean Journal of Aerospace*, 46(3), 189-196. https://doi.org/10.5139/JKSAS.2018.46.3.189
Chen, Y., Liu, P., Tang, Z. & Guo, H. (2015). Wind tunnel tests of stratospheric airship counter rotating propellers. *Theoretical and Applied Mechanics Letters*, 5(1), 58-61. https://doi.org/10.1016/j.taml.2015.01.001
Ciliberti, D. & Nicolosi, F. (2022). Design, analysis, and testing of a scaled propeller for an innovative regional turboprop aircraft. *Aerospace*, 9(5), 264. https://doi.org/10.3390/aerospace9050264
Czyż, Z., Karpinski, P. & Skiba, K. (2021). Wind tunnel investigation of the propellers for unmanned aerial vehicle. *2021 IEEE International Workshop on Metrology for Aerospace*, 672-676. https://doi.org/10.1109/MetroAeroSpace51421.2021.9511724
Czyż, Z., Karpinski, P. & Skiba, K. (2022). Wind tunnel performance tests of the propellers with different pitch for the electric propulsion system. *Sensors*, 22(1), 2. https://doi.org/10.3390/s22010002
Czyż, Z., Karpinski, P. & Stryczniewicz, W. (2020). Measurement of the flow field generated by multicopter propellers. *Sensors*, 20(19), 5537. https://doi.org/10.3390/s20195537
Deters, R.W., Ananda, G.K. & Selig, M.S. (2014). Reynolds number effects on the performance of small-scale propellers. *Journal of Aircraft*, 51(4), 1234-1245. https://doi.org/10.2514/1.C032267
Fischer, A. & Müller, B. (2021). *Advanced Aerodynamics and UAV Performance Optimization*. Aviation Publishers.
Giguere, P., Lemay, J. & Dumas, G. (1995). Gurney flap effects and scaling for low-speed airfoils. *13th Applied Aerodynamics Conference*, 1881. https://doi.org/10.2514/6.1995-1881
Go, Y.J., Kim, D.H., Lee, J.W. & Lee, D.H. (2022). A study on the scale effect according to the Reynolds number in propeller flow analysis and a model experiment. *Aerospace*, 9(10), 559. https://doi.org/10.3390/aerospace9100559
Gur, O. & Rosen, A. (2009). Flight performance and propulsion systems: Advanced topics. *Aviation Research Journal*, 34(2), 123-136. https://doi.org/10.1016/j.avr.2009.01.002
Hassinalian, M. & Abdelkefi, A. (2017). Classification, applications, and design of drones: A review. *Progress in Aerospace Sciences*, 91, 99-131. https://doi.org/10.1016/j.paerosci.2017.04.003
Kutty, H.A., Rajendran, P. & Mule, A. (2017). Performance analysis of small scale UAV propeller with slotted design. *2017 International Conference on Innovations in Information, Embedded and Communication Systems*, 695-700. https://doi.org/10.1109/I2CT.2017.8226219
Liu, X., Zhao, D. & Oo, N.L. (2023). Comparison studies on aerodynamic performances of a rotating propeller for small-size UAVs. *Aerospace Science and Technology*, 133, 108148. https://doi.org/10.1016/j.ast.2023.108148
Moreira, C., Herzog, N. & Breitsamter, C. (2024). Wind tunnel investigation of transient propeller loads for non-axial inflow conditions. *Aerospace*, 11(4), 274. https://doi.org/10.3390/aerospace11040274
Murakami, M., Saito, Y. & Aono, H. (2022). Effects of gusty flow on aerodynamic performance of multirotor drone propellers in hovering flight. *Journal of Fluid Science and Technology*, 17(4), JFST0013. https://doi.org/10.1299/jfst.2022jfst0013
Pobikrowska, K. & Goetzendorf-Grabowski, T. (2021). Wind tunnel tests of hovering propellers in the transition state of Quad-Plane. *Bulletin of the Polish Academy of Sciences: Technical Sciences*, 69(6), e138821. https://doi.org/10.24425/bpasts.2021.138821
Podsedkowski, M., Lipian, M. & Obidowski, D. (2023). Variable pitch propeller - blade pitch moment computational analysis. *2023 International Conference on Unmanned Aircraft Systems*, 118-122. https://doi.org/10.1109/ICUAS57906.2023.10155835
Quach, H.V., Nguyen, T.T. & Kim, S.J. (2024). Analysis and evaluation of aerodynamic characteristics of super-heavy drone. *Transportation Research Procedia*, 80, 186-194. https://doi.org/10.1016/j.trpro.2024.09.024
Raffel, M., Willert, C.E., Wereley, S.T. & Kompenhans, J. (2006). Micro-PIV and ELDV wind tunnel investigations of the laminar separation bubble above a helicopter blade tip. *Measurement Science and Technology*, 17, 1652-1658. https://doi.org/10.1088/0957-0233/17/7/006
Romeo, G., Borello, F., Correa, G. & Cestino, E. (2012). Design and testing of a propeller for a two-seater aircraft powered by fuel cells. *Journal of Aerospace Engineering*, 226(8), 804-816. https://doi.org/10.1177/0954410011417440
Simmons, B.M. & Hatke, D.B. (2021). Investigation of high incidence angle propeller aerodynamics for subscale eVTOL aircraft. *NASA Technical Memorandum*, 20210014010.
Smith, J. & Johnson, R. (2018). Kriyojenik rüzgâr tünellerinde yüksek Reynolds sayılarına ulaşma yöntemleri. *Journal of Aerospace Engineering*, 45(3), 123-135. https://doi.org/10.1016/j.jaes.2018.05.010
Theys, B., Dimitriadis, G., Andrianne, T. & De Schutter, J. (2014). Wind tunnel testing of tilted MAV propeller. *2014 International Conference on Unmanned Aircraft Systems*, 1064-1072. https://doi.org/10.1109/ICUAS.2014.6842357
Theys, B., Dimitriadis, G., Andrianne, T. & De Schutter, J. (2016). Influence of propeller configuration on propulsion system efficiency of multi-rotor UAVs. *2016 International Conference on Unmanned Aircraft Systems*, 195-201. https://doi.org/10.1109/ICUAS.2016.7502664
Vogeltanz, T. (2016). Performance analysis of mini-propellers based on FlightGear. *AIP Conference Proceedings*, 1738, 480086. https://doi.org/10.1063/1.4951902
Xiang, S., Liu, Z., Zhang, Y. & Li, J. (2018). An improved propeller design method for the electric aircraft. *Aerospace Science and Technology*, 78, 488-493. https://doi.org/10.1016/j.ast.2018.05.008
Yao, Y., Zhang, Y., Chen, H. & Li, Q. (2022). Aerodynamic optimization and analysis of low Reynolds number propeller with Gurney flap for ultra-high-altitude unmanned aerial vehicle. *Applied Sciences*, 12(6), 3195. https://doi.org/10.3390/app12063195

Ayrıntılar

Birincil Dil

Türkçe

Konular

Makine Mühendisliği (Diğer)

Bölüm

Derleme

Yazarlar

Şükrü Eldek ^*
0009-0003-5781-1509
Türkiye

Selim Tangöz
0000-0002-8284-1326
Türkiye

Yayımlanma Tarihi

3 Aralık 2025

Gönderilme Tarihi

30 Nisan 2025

Kabul Tarihi

5 Kasım 2025

Yayımlandığı Sayı

Yıl 2025 Cilt: 28 Sayı: 4

DOI

https://doi.org/10.17780/ksujes.1687992

IZ

https://izlik.org/JA33UW25DG

Kaynak Göster

RIS / Bibtex

APA

Eldek, Ş., & Tangöz, S. (2025). FARKLI YÖNDEN GELEN RÜZGÂRIN İHA MOTOR PERVANESİ ÜZERİNDEKİ ETKİSİ: BİR DERLEME. Kahramanmaraş Sütçü İmam Üniversitesi Mühendislik Bilimleri Dergisi, 28(4), 2161-2176. https://doi.org/10.17780/ksujes.1687992