Wing curvature, or camber, significantly influences lift generation in an airfoil. A wing with a curved upper surface creates a pressure difference between the upper and lower surfaces as air flows over it, resulting in increased lift. The greater the curvature, the more pronounced this effect, especially at specific angles of attack. However, if the angle of attack becomes too steep, it can lead to airflow separation and stall, reducing lift.
When the curvature of the wing increases, air moving across the top of the wing moves more rapidly. The increased difference in speed between the air above the wing and the air below the wing will help to cause an increased lift on the wing.
The camber on a wing refers to the curvature of the wing. A high camber means the wing is thick and produces more lift but flies slower. A low camber means the wing is thinner, produces less lift but flies much faster.
Upper camber refers to the curvature or arch of the upper surface of an airfoil or wing. This design feature affects the airflow over the wing, contributing to lift generation. A greater upper camber typically enhances lift at lower speeds, while different camber profiles can influence the aerodynamic efficiency and performance characteristics of the aircraft.
Shape as in the curvature of the wing (camber), Size as in the wing's size, Speed,Thrust , the weight of the aircraft, may be drag too.
the wing flap
They help produce more lift by the wing. Lift is dependant on the formula L=CL x1/2densityx speed (squared) xsurface area So the greater the surface area the more lift produced. Flaps can extend from the front of the back of the wing. They also change the curvature of the wing thus producing more lift as well. They are used for takeoff and landing because they allow the wing to produce more lift at a slower speed.
The wing shape of an airplane, particularly its airfoil profile, affects its ability to generate lift. A curved or cambered wing shape helps generate more lift, allowing the airplane to carry more weight. Additionally, the wing design influences the distribution and efficiency of lift across the wingspan.
Lift is an aerodynamic force that results from the air passing over the curvature of the wing. It causes a reaction. A high pressure on the bottom of the wing and a lower pressure on top of the wing. As a result, high pressure wants to go to low pressure and so the wind is lifted into the air. Drag is the force opposite to thrust. It is created by the airplane as it moves through the air. The faster the airplane, the more the drag.
That would be the flaps. There are flaps on the trailing edge of a wing on most aircraft and there can also be leading edge flaps as well, often seen on the big airliners. These flaps will be lowered and will effectively increase the curvature of the wing, allowing it fly at higher angles of attack for greater lift. It also produces greater drag, useful for dropping altitude without speeding up and flying slow on approach to landing.
In mathematics curvature affects extent to which a shape deviates from being flat, even or straight.
The best way to answer this question would be to say what does effect the lift of a wing. Pretty much the only things that effect the lift of a wing are the density of the air over the wing, the surface area of the wing, the speed of air over the wing and the angle of attack. Everything else has no effect on the amount of lift on a wing.
The angle of a wing as it meets the airflow is called the "angle of attack." This angle is crucial for generating lift; as the angle increases, lift typically increases up to a certain point, beyond which airflow can separate from the wing, leading to stall. The angle of attack is a key parameter in aerodynamics and affects the performance and stability of an aircraft.