한국항공운항학회지 (Journal of the Korean Society for Aviation and Aeronautics)

  • 제30권4호
  • /
  • Pages.57-64
  • /
  • 2022
  • /
  • 1225-9705(pISSN)
  • /
  • 2466-1791(eISSN)
한국항공운항학회 (The Korean Society for Aviation and Aeronautics)
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무인항공기용 프로펠러 형상에 따른 추력특성 해석

Analysis of Thrust Characteristics with Propeller Shape for UAV

  • 이수현 (청주대학교 융합신기술대학원) ;
  • 조환기 (청주대학교 항공학부 항공운항학과)
  • 투고 : 2022.08.11
  • 심사 : 2022.11.24
  • 발행 : 2022.12.31
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초록

A study on propllers for unmaned aerial vehicles is conducted using the open softwares. Since the shape of the propeller is closely related to the thurst characteristics of the propulsion system, adopting an appropriate propeller will significantly reflect stable aerodynamic performances. In this study, propellers for unmanned aerial vehicles were modeled by using OpenVSP and Propel for comparison, the thrust characteristics according to the number of blades and the diameter of the propeller were analyzed. In addition, the tendency of thrust characteristics according to various propeller pitch angles was confirmed. Based on the analysis results of this study, the applicability of the propeller shape to the design of the unmanned aerial vehicle was confirmed. It is shownthat the analysis results of this study can be utilized when modeling the propeller shape in research such as a conceptual design of unmanned aerial vehicle. In this case, it should be noted that OpenVSP does not involve the viscous effect of air.

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참고문헌

  1. Ahn, J., Jang, B., Kim, J., Hwang, H., Hyun, J., Ko, H., Hong, Y., and Oh, J., "Optimal design of the propeller and electric propulsion system for a solar powered high altitude long endurance UAV", 2015 KSAS Conference, The Korean Society for Aeronautical & Space Sciences, 2015, pp.598-601.
  2. Ahn, J., Park, S., and Woo, R., "Optimized design and performance analysis of a propeller for an electric powered mini UAV", 2014 KSAS Conference, The Korean Society for Aeronautical & Space Sciences, 2014, pp.209-212.
  3. Kim, S., and Lee, S., "Structural sizing for optionally piloted PAV preliminary design", Journal of the Korean Society for Aviation and Aeronautics, 28(1), 2020, pp.83-89. https://doi.org/10.12985/ksaa.2020.28.1.083
  4. Patel, Y., Anant, G., Krovvidi, S., and Yamal, S., "A review on design and analysis of the propeller used in UAV", International Journal of Advanced Production and Industrial Engineering, 605, 2017, pp.20-23.
  5. Eraslan, Y., Ozen, E., and Oktay, T., "A literature review on determination of quadrotor unmanned aerial vehicles propeller thrust and power coefficients", EJONS 10th International Conference on Mathematics Engineering, Natural & Medical Sciences, 2020, pp.108-118.
  6. Podsedkowski, M., Konopinski, R., Obidowski, D., and Koter, K., "Variable pitch propeller for UAV-experimental tests", Energies, 13(20), 5264, 2020, pp.1-16.
  7. Czyz, Z., Karpinski, P., Skiba, K., and Wendeker, M., "Wind tunnel performance tests of the propellers with different pitch for the electric propulsion system", Sensors, 22(2), 2022, pp.1-18. https://doi.org/10.1109/JSEN.2021.3136033
  8. Cruzatty, C., Sarmiento, E., Valencia, E., and Cando, E., "Design methodology of a UAV propeller implemented in monitoring activities", Materialstoday: Proceedings, 49, 2022, pp.115-121.
  9. Oktay, T., and Eraslan, Y., "Numerical investigation of effects of airspeed and rotational speed on quadrotor UAV propeller thrust coefficient", Journal of Aviation, 5(1), 2021, pp.9-15. https://doi.org/10.30518/jav.872627
  10. Brandon, L., and Kinsey, R., "VSP Aircraft Analysis User Manual", NASA, 2014.
  11. Edwin, P. H., and David, B., "The aerodynamic characteristics of full-scale propellers having 2, 3 and 4 blades of Clark Y and R. A. F. 6 airfoil sections", Report No. 640, Langley Memorial Aeronautical Laboratory, National Advisory Committee for Aeronautics, Langley Field, VA., November 9, 1937.
  12. Xia, X., Ma, D., Zhang, L., Liu, X., and Cong, K., "Blade shape optimization and analysis of a propeller for VTOL based on an inverse method", Applied Sciences, 12(7), 2022.
  13. Edwin, P. H., and David, B., "Tests of two full-scale propellers with different pitch distributions, at blade angles up to 60°", Report No. 658, Langley Memorial Aero-nautical Laboratory, National Advisory Committee for Aeronautics, Langley Field, VA., Apr. 14, 1938.