Analysis of Thrust Characteristics with Propeller Shape for UAV

Author:

Lee Soohyeon,Cho Hwankee

Publisher

The Korean Society for Aviation and Aeronautics

Subject

General Medicine

Reference13 articles.

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. 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.

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