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Calculate Static Thrust of Turbojet Engine Method to Calculate the Static Thrust of a Turbojet Engine 

Aerospace



Static Thrust of a Turbojet Engine In order to calculate the Static Thrust of a Turbojet Engine we have assumed that the Turbojet Engine is mounted on a stationary test stand at sealevel. 

For the calculation of static thrust we require,
The inlet area and exit area of turbojet engine in m^2. The velocity at exit of Turbojet engine in m/s The pressure at exit of Turbojet engine Pe in N/m^2. The temperature at exit of the turbojet engine in K.
Using the Thrust equation and the equation of continuity with the assumption that V(infinity) = 0, the Static Thrust of the turbojet engine is computed. 

Download Free Program to Calculate the Static Thrust of a Turbojet Engine

