In flight mechanics, thrust refers to the force generated by an aircraft’s propulsion system, typically provided by engines or jet turbines. It acts in the direction of the aircraft’s motion and counteracts the resistance forces, such as drag. Thrust is a crucial parameter in achieving and maintaining controlled flight, influencing an aircraft’s speed, altitude, and overall performance. The formula to calculate Thrust as follows:
Where:
- W is the Weight in N
- g is the gravity in m/s2.
- ρ∞ is the density in kg/m3.
- S is the wing area in m2.
- CLmax is the Maximum Lift Coefficient.
- SLO is the Liftoff distance in m.