EFD and CFD Characterization of a CLT Propeller

Figure 15

Axial, tangential, and radial vorticity distributions at 𝑥/𝑅 = 0.4875, 𝑟/𝑅 = 0.60, and 𝑟/𝑅 = 0.80. Comparison between LDV and RANSE (single-blade angular sector).

(a)

(b)