Research Article
Efficacy Analysis of Thickness and Camber Size of Cross Section of the Stator on Hydrodynamic Parameters in Linear Jet Propulsion System
Table 7
Thrust, torque, and efficiency for different thickness distributions in J = 1.6.
| | Thickness | Thrust of rotor (N) | Thrust of stator (N) | Thrust of duct (N) | Total thrust (N) | Torque of rotor (N-m) | Efficiency |
| | NACA0010 | 176.087 | −0.659 | −67.878 | 107.548 | 11.626 | 47.113 | | NACA0015 | 176.727 | −0.800 | −62.074 | 113.852 | 11.642 | 49.806 | | NACA0020 | 177.450 | −10.811 | −56.221 | 110.416 | 11.689 | 48.105 |
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