Airfoil

Explanation

Airfoils are the characteristic shapes of any wings, propeller blades, compressor or turbine blades in an aircraft. This shape produces the aerodynamic force needed for an aircraft as it moves through the air at a certain angle, called angle of attack. The lift is this aerodynamic force's perpendicular component to the direction of motion, and the parallel component is called as drag. The airfoil shape is what makes the wings produce an efficient lift, by minimizing the drag. The lift produced by an airfoil can be explained by Newton's third law and Bernoulli's principle. As the airfoil moves at a certain angle, it deflects the air downwards, producing an equal magnitude of force in the opposite direction, resulting in lift and drag respectively. In addition to this, the airfoil shape is responsible for pressure differences on the top and bottom of a wing. The upper surface of an airfoil has high-velocity air with a low potential energy and thereby less static pressure. Conversely, on the lower surface, there is a low-velocity region formed with increased static pressure. This pressure difference creates lift due to the Bernoulli's principle. However, the precise explanation of lift due to airfoil has been debated due to the limitations of the theories.

Frequently Asked Questions

What is stalling?

Stalling is an aerodynamical situation in a typical fixed-wing aircraft, where the wings will stop producing required lift. This happens mostly when the angle of attack of an aircraft increases beyond the critical angle of attack, which is also called as the stalling angle of attack. Sometimes, a stall can happen when there is not enough airspeed for an aircraft to generate lift. Most stalls can be recovered by pitching the nose of the aircraft down, thereby reducing the angle of attack. However, in the case of deep stalls, a dangerous stall where a stalled wing pitches the plane up and masks any airflow to its tail section, the recovery will be hard as the elevators will not be able to help the pilot in pitching down the plane. As there is no lift produced by the wings during a stall, the altitude drops usually and it is always a crucial factor for a recovery maneuver.