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Abstract

Previous studies at HCMUT have been carried out on free propellers in static condition for Unmanned Aerial Vehicle (UAV), not much data exists for ducted propellers. According to theory, the ducted propeller has some better characteristics than than the free propeller. The paper presents an experimental design, based on load-cell deformation, for the small ducted propeller. The experimental model will be carried out for the Master Airscrew E9x6 propeller in the case with duct and without duct, in the static condition. The results obtained will be compared with the manufacturer's results (conducted by the University of Illinois, without duct, in static condition), and compared to the numerical simulation results. From there, choose the kind of propeller that match the design of the UAV.



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Article Details

Issue: Vol 20 No K3 (2017)
Page No.: 60-66
Published: Jun 30, 2017
Section: Engineering and Technology - Research article
DOI: https://doi.org/10.32508/stdj.v20iK3.1093

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Creative Commons License

Copyright: The Authors. This is an open access article distributed under the terms of the Creative Commons Attribution License CC-BY 4.0., which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.

 How to Cite
Nguyen, N., & Ngo, H. (2017). Experimental study on static thrust characteristics of Master Airscrew E9x6 propeller with duct. Science and Technology Development Journal, 20(K3), 60-66. https://doi.org/https://doi.org/10.32508/stdj.v20iK3.1093

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