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Revision as of 19:06, 25 April 2017 by Editor1
|Category:||Theory of Flight|
Aerofoil or Airfoil
A body shaped to produce an aerodynamic reaction (lift) perpendicular to its direction of motion, for a small resistance (drag) force in that plane.
The airflow over the wing increases its speed causing a reduction in pressure; this generates a force (lift) perpendicular to the chord of the aerofoil. The airflow below the wing moves much more slowly generating greater pressure and less or negative lift. See the article Bernoulli's Principle for further information.
All aerofoil surfaces generate drag.
The distance between a wing root and wing tip the length of the wing. Wing span is the distance from one wing tip to the other wing tip. The ratio of wing length to chord is called the aspect ratio.
The objective of aerofoil design is to achieve the best compromise between lift and drag for the flight envelope in which it is intended to operate.
Aerofoil surfaces includes wings, tailplanes, fins, winglets, propeller blades and helicopter rotor blades. Control surfaces (e.g. ailerons, elevators and rudders) are shaped to contribute to the overall aerofoil section of the wing or empennage.