- Dom, 28 Nov 2010 21:25
#1000496
siento disentir de nuevo, no es por entrar en polemicas pero :
saludos
en lo demas totalmente de acuerdo con lo dichoWashout refers to a feature of wing design to deliberately reduce the lift distribution across the span of the wing of an aircraft. The wing is designed so that lift is strongest at the wing roots and decreases across the span, becoming weakest at the wing tip. This is usually to ensure that, at the stall, the wing root stalls before the wing tips, providing the aircraft with some resistance to spinning. Washout may also be used to modify the spanwise lift distribution to reduce lift-induced drag.
Washout is commonly achieved by designing the wing with a slight twist, reducing the angle of incidence from root to tip, and therefore causing a lower angle of attack at the tips than at the roots. This is sometimes referred to as structural washout, to distinguish it from aerodynamic washout.
Wingtip stall is unlikely to occur symmetrically, especially if the aircraft is maneuvering. As an aircraft turns, the wing tip on the inside of the turn is moving more slowly and is most likely to stall. As an aircraft rolls, the down-going wing tip is at higher incidence and is most likely to stall. When one wing tip stalls it leads to wing drop, a rapid rolling motion.
From Wikipedia.
saludos
Bonnie Tyler ( estara pensando en aeromodelismo ) ;-))
https://www.youtube.com/watch?v=3cGXOkN4NCo
https://www.youtube.com/watch?v=3cGXOkN4NCo