Analysis of a Propeller

Your virtual propeller design can be analyzed at off-design conditions, i.e. at a different speed or a different velocity of rotation. The analysis is a so called "Blade Element Method" and uses the same airfoil polars as the design procedure. The influence of blade number and tip loss are take into account by the "Prandtl Tip-Loss Factor". More details can be found in references [10] and [11]. It should be noted, that the analysis does not work accurately for high thrust loadings as they occur under static conditions. 

JavaProp offers two ways to use the analysis procedure:

Last modification of this page: 21.05.18

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