In flight mechanics, the thrust angle refers to the angle at which the thrust vector of an aircraft’s propulsion system is oriented in relation to the aircraft’s longitudinal axis. It plays a crucial role in determining the aircraft’s directional stability and control during flight. Proper alignment of the thrust angle is essential for balanced and efficient performance, as deviations can impact the aircraft’s trim and handling characteristics. The formula to calculate Thrust angle is as follows:
Where:
- σT is the Thrust angle in radian.
- D is the Drag force in N
- T is the Thrust in N.