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

Figure 19

Pressure coefficient distribution in different cambers of stator at J = 1.6. (a) Span = 0.03. (b) Span = 0.06. (c) Span = 0.09.

(a)

(b)

(c)