Affiliation
Univ Arizona, Dept Aerosp & Mech EngnIssue Date
2019-12-22
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SAGE PUBLICATIONS LTDCitation
Zhao, L., & Shkarayev, S. (2019). Characterization of ducted contra-rotating propeller propulsions. International Journal of Micro Air Vehicles, 11, 175682931983766. https://doi.org/10.1177/1756829319837661 Rights
Copyright © The Author(s) 2019. This article is distributed under the terms of the Creative Commons AttributionNonCommercial 4.0 License (http://www.creativecommons.org/licenses/by-nc/4.0/).Collection Information
This item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.Abstract
This paper presents the experimental studies of the efficiency of open and ducted contra-rotating propeller systems operating in the low Reynolds number range. Eight off-the-shelf propellers were selected with a diameter in the range from 139 mm to 377 mm and seven ducts were built with the duct length of 0.28–0.53 the propeller diameter. Static and wind tunnel experiments were conducted. The maximum increase in the static thrust coefficient and power loading for the ducted contra-rotating propeller systems over the open systems was found to be 25% and 50%, respectively. This performance improvement for the medium size ducted systems is smaller than that observed in previous studies for ducts longer than the 0.8 propeller diameter but greater than for ducts shorter than the 0.15 propeller diameter. The thrust coefficient decreases with an advance ratio increase. The power loading of both open and ducted systems drops dramatically after reaching maxima.Note
Open access journalISSN
1756-8293Version
Final published versionae974a485f413a2113503eed53cd6c53
10.1177/1756829319837661
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Except where otherwise noted, this item's license is described as Copyright © The Author(s) 2019. This article is distributed under the terms of the Creative Commons AttributionNonCommercial 4.0 License (http://www.creativecommons.org/licenses/by-nc/4.0/).

