Abstract
A detailed aerodynamic study of a 'humpy' high-speed propeller is presented. This propeller is the result of a bi-disciplinary optimisation procedure and features blade segments of wider chord bordered by narrow segments. The aerodynamic consequences of these regions are investigated and correlated to the aeroacoustic properties by comparison to an equivalent blade without hump. Copyright © 2012 Inderscience Enterprises Ltd.
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APA
Marinus, B. G., Bosschaerts, W., & Roger, M. (2012). Aerodynamic study of a “humpy” propeller. International Journal of Engineering Systems Modelling and Simulation, 4(1–2), 27–35. https://doi.org/10.1504/IJESMS.2012.044841
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