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

Figure 17

Camber effect on streamlines around rotor and stator at J = 1.6. (a) Streamlines of NACA0015. (b) Streamlines of NACA3515. (c) Streamlines of NACA6515. (d) 2D Streamlines of NACA0015 after stator. (e) 2D streamlines of NACA3515 after stator. (f) 2D streamlines of NACA6515 after stator.

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