The wings of an aircraft are designed to generate lift, which is the force that opposes gravity and allows the aircraft to fly.

Camber is the curved shape of an aircraft's wing, which helps to generate lift.

The fuselage of an aircraft is the main body of the aircraft, which houses the passengers and crew.

The horizontal stabilizer is the horizontal tail surface of an aircraft, which helps to provide stability and control.

The engine of an aircraft is responsible for generating thrust, which is the force that propels the aircraft forward.

Sweep is the angle at which an aircraft's wing is swept back.

Ailerons are the primary flight control surfaces that provide roll control for an aircraft.

Aspect ratio is the ratio of an aircraft's wingspan to its wing chord.

The rudder is the primary flight control surface that provides yaw control for an aircraft.

Dihedral is the angle at which an aircraft's wing is tilted upward.

The elevator is the primary flight control surface that provides pitch control for an aircraft.

Lift-to-drag ratio is the ratio of an aircraft's lift to its drag.

Flaps are used to increase lift, typically during takeoff and landing.

Propeller pitch is the angle at which an aircraft's propeller is tilted upward.

Slats are used to increase lift, typically during takeoff and landing.