Simplified propeller analysis and design including effects of stall
A simplified method to analyse propellers based on vortex theory is presented. Small-angle approximations are implemented to eliminate the need for iteration in the determination of the induced angle-of-attack. A stall model is developed and combined with analytic relations describing the blade aero...
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Published in | Aeronautical journal Vol. 120; no. 1227; pp. 796 - 818 |
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Main Author | |
Format | Journal Article |
Language | English |
Published |
Cambridge, UK
Cambridge University Press
01.05.2016
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Subjects | |
Online Access | Get full text |
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