International Journal of Rotating Machinery / 2012 / Article / Fig 17

Research Article

EFD and CFD Characterization of a CLT Propeller

Figure 17

Axial, tangential, and radial vorticity distributions at = 0.5000 aft the propeller plane. ((a), (c), and (e)) Experimental LDV measurements. ((b), (d), and (f)) RANSE computations on the finer mesh.
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