Abstract
Thrust Benchmarking System (TBS), a low cost and easy to manufacture instrument for electric UAV propulsion system performance measurement is being proposed. With one of its uses for determining the static thrust of a propeller based on simple empirical characterization modeling. In this paper, characteristic modeling is performed on 3 APC-Electric propellers with different pitch and diameter dimensions. As a result, there are 2 constants K1 and K2 which can express similar propeller characteristics with different dimensions. It costs IDR 1.6 million and took two-and-a-half months of manufacture and assembly process.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
