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NTIS 바로가기한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.50 no.1, 2022년, pp.1 - 12
신수희 (Dept. of Aerospace System Engineering, Korea University of Science and Technology) , 이승훈 (Korea Aerospace Research Institute) , 김양원 (Korea Aerospace Research Institute) , 조태환 (Dept. of Aerospace System Engineering, Korea University of Science and Technology)
Wind tunnel test for a small scale electric ducted fan with a 104mm diameter was conducted to analyze the aerodynamic characteristics when it was used as a propulsion system of tilt-propeller UAV. Experimental conditions were derived from flight conditions of a sub-scaled OPPAV. Forces and moments o...
Wang, B., Guo, Z., Wang, P., Shan, S. and How, X., "Investigation of the Aerodynamic Characteristics of Ducted Fan System," World Academy of Science, Engineering and Technology, Vol. 6, 2012.
Park, Y. M., Bang, H. S., Jeong, J. D. and Lee, H. C., "Comparison of Ducted Fan and Rotor Aerodynamic Performances for VTOL UAV," Proceeding of The Korean Society for Aeronautical and Space Science Fall Conference, November 2014, pp. 1055~1058.
Akturk, A., Shavalikul, A. and Camci, C., "PIV Measurement and Computational Study of a 5-inch Ducted Fan for V/STOL UAV Applications," 47th AIAA Aerospace Sciences Meeting and Exhibit, Orlando, Florida, January 2009.
Anita, I. and Robert, W., "Performance Study of a Ducted Fan System," American Helicopter Society Aerodynamics, Acoustics, and Test and Evaluation Technical Specialists Meeting, 2002.
Choi, S. W., "Configuration design and performance analysis for the sub-scaled OPPAV," Proceeding of The Korean Society for Aeronautical and Space Science Fall Conference, November 2019, pp. 629~630.
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