EFD and CFD Characterization of a CLT Propeller

Figure 17

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