Efficacy Analysis of Thickness and Camber Size of Cross Section of the Stator on Hydrodynamic Parameters in Linear Jet Propulsion System

Figure 5

Grid structure in numerical solution for ka4.70, P/D = 1, and duct 19A. (a) Elements on the surface of the propeller and hub. (b) Side view of grids around the propeller. (c) Front view of grids around the propeller. (d) Boundary layer around propeller and inside the tip clearance.

(a)

(b)

(c)

(d)