International Journal of Rotating Machinery / 2012 / Article / Fig 10

Research Article

A Wake Model for the Prediction of Propeller Performance at Low Advance Ratios

Figure 10

Radial location of tip vortex for propeller DTMB 4119 at design (0.833), from different values of , the triangles represent the experimental measurement by Jessup [9].

Article of the Year Award: Outstanding research contributions of 2020, as selected by our Chief Editors. Read the winning articles.