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].
372364.fig.0010a
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372364.fig.0010b
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