EFD and CFD Characterization of a CLT Propeller

Figure 16

Axial, tangential, and radial vorticity distributions at 𝑥/𝑅 = 0.4875, 𝑟/𝑅 = 0.85, and 𝑟/𝑅 = 0.90. Comparison between LDV and RANSE (single blade angular sector).

(a)

(b)