Calculate Thrust of a Turbojet Engine

 Method to Calculate the Thrust of a Turbojet Engine

• Calculate Power Available of Internal Combustion Engine

• Calculate Mean Effective Pressure of Internal Combustion Engine

• Calculate Thrust of Rocket Engine at Standard Altitude

• Calculate Pressure in the Combustion Chamber of a Rocket Engine

• Calculate Thrust of a Turbojet Engine

• Calculate Static Thrust of a Turbojet Engine

• Calculate Gas Temperature at Exit of Turbojet Engine

• Calculate Inlet Area of Ramjet Engine

• Calculate Burnout Velocity of Single Stage Rocket

• Calculate Burnout Velocity of Double Stage Rocket

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

Aerospace

 Aerospace

 Aerospace Engineering

 Aeronautical Engineering

 Aeronautics

 Astronautics

 Space Exploration

 Aerospace Industry

 Aerospace Related Questions

 Aerospace Related Articles

Thrust of a Turbojet Engine

In order to calculate the thrust of a turbojet engine we must know the altitude at which the airplane is flying in meters m.

Also, we neet the Velocity of the Airplane in meters/sec.

The Inlet Area of a Turbojet engine and

the Exit Area of the Turbojet engine in meter^2

Furthermore, we also require the Velocity of the Exhaust Gas at the Exit in m/s and the Pressure of the Exhaust gas in N/m^2.

Performing the calculation,

Using the Thrust equation for the Turbojet engine and the equation of continuity the thrust is computed.

Download Free Program to Calculate the Thrust of a Turbojet Engine