Thrust Coefficient For a Turbojet Engine Calculator

The thrust coefficient for a turbojet engine is a dimensionless parameter that relates the thrust produced by the engine to the dynamic pressure of the incoming air. It is a measure of the efficiency of the propulsion system in converting fuel into thrust.

The thrust coefficient is defined as the ratio of the thrust force produced by the propulsion system to the dynamic pressure of the incoming air. Mathematically, it is expressed as:

where,

where:

• C_T​ is the thrust coefficient,
• $T$ is the thrust force,
• $\rho$ is the air density,
• $V$ is the airspeed,
• $A$ is the reference area.