Question

What forces and moments contribute to the pitching moment equation for a conventional aircraft?

1) Lift force and drag force
2) Thrust force and weight force
3) Rolling moment and yawing moment
4) Pitching moment and rolling moment

Answer 1

The pitching moment equation for a conventional aircraft includes lift force, drag force, pitching moment, and rolling moment.

Step-by-step explanation:

The pitching moment equation for a conventional aircraft involves various forces and moments. The forces and moments that contribute to the equation are:

1. Lift force: This is the upward force generated by the wings of the aircraft as a result of the airflow over them.
2. Drag force: This is the force that opposes the motion of the aircraft through the air.
3. Pitching moment: This is the moment that causes the aircraft to rotate around its lateral (pitch) axis.
4. Rolling moment: This is the moment that causes the aircraft to rotate around its longitudinal (roll) axis.