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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Bibliographic Details
Published inAeronautical journal Vol. 120; no. 1227; pp. 796 - 818
Main Author Traub, L.W.
Format Journal Article
LanguageEnglish
Published Cambridge, UK Cambridge University Press 01.05.2016
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