Pilot Institute

JUNE 4, 2025

The Weather Vane It mostly comes from the vertical stabilizer (fin) and the sides of the fuselage behind the center of gravity. The reflexed shape of the airfoil usually causes a positive (nose-up) pitching moment coefficient at its aerodynamic center. Upward Deflection : Raising both elevons decreases the camber of the wing.

Tail 52

Tail Airplanes Weight-Shift-Control Drag 52

Pilot Institute

FEBRUARY 20, 2025

The asymmetry between the top and bottom surface of the wing is called wing camber. The downward movement of the aileron increases the asymmetry and, therefore, the camber while raising the aileron reduces the wing camber. This shifts the ailerons Center of Gravity (C.G.) What Is Aircraft Stability?

Aileron 90

Aileron Weight-Shift-Control Rudder Longitudinal Axis 90

Pilot Institute

APRIL 12, 2025

This principle is fundamental in generating lift, thrust, and maneuverability, allowing aircraft to fly. Thrust (how it moves forward). One is the upper wing surfaces curvature compared to the lower surface, called wing camber. That force is called thrust. Thrust relies on Newtons Third Law as well.

Lift 52

Lift Torque Thrust Aileron 52