Caided
Tab7 - Thrusts
Click the view menu and check the Thrusts option to display the thrust tab
The intake momentum is calculated from the flights conditions and intake mass flow rate.
The core gross thrust is derived from the nozzle page.
A bypass gross thrust is derived from the engine page with the Turbofan setting switched on.
The net thrust can then be calculated and displayed.
Click the view menu and check the Thrusts option to display the thrust tab
The intake momentum is calculated from the flights conditions and intake mass flow rate.
The core gross thrust is derived from the nozzle page.
A bypass gross thrust is derived from the engine page with the Turbofan setting switched on.
The net thrust can then be calculated and displayed.
