Aerodynamic parameters | Case 1 | Case 2 | Case 3 |
Compressed air inlet mass flow rate (kg/s) | 0.255 | 0.246 | 0.244 |
Rotor nozzle total pressure (MPa) | 0.121 | 0.121 | 0.121 |
Rotor nozzle total temperature (K) | 418.12 | 435.43 | 437.33 |
Rotor nozzle absolute velocity/(m/s) | 203.77 | 204.25 | 203.01 |
Rotor nozzle mass flow rate (kg/s) | 0.295 | 0.286 | 0.284 |
Available moment (N∙m) | 92.37 | 89.59 | 88.27 |