Calculate Static Thrust of Turbojet Engine

 Method to Calculate the Static Thrust of a Turbojet Engine

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• Calculate Gas Temperature at Exit of Turbojet Engine

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• Calculate Burnout Velocity of Double Stage Rocket

• Calculate Ratio of Initial Mass to Final Mass of a Rocket

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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 sea-level.

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