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

Table 6

Conditions of inlet flow to computational domain around the linear jet propulsion system.

Advance ratio (J)	Inlet velocity (m/s)	n (rpm)
1.4	4	857.14
1.6	4	750
1.8	4	666.66
2	4	600