by ADW 123 » Tue May 31, 2011 3:11 pm
64 eehh? im 14, but who said young cant teach the old?
On fixed-wing aircraft, angle of incidence is the angle between the chord line of the wing where the wing is mounted to the fuselage and the longitudinal axis of the fuselage. The angle of incidence is fixed in the design of the aircraft by the mounting of the wing to the fuselage.
essentialy, what i described in those pictures is just changing the angle of incidence at the wing tips. the greater the angle, the more washout. the more washout there is, the less lift that side of the wing generates.
if you want the trim for a turn for rubber FF, you might notice that the rudder alone will cause the plane's wing to dip to the inside of the turn. this can be very bad, and most of the time fatal if the wing hits the ground like that.
adding the some washout on the left wing, and a little more on the right (called differential washout) and some left rudder, will cause the left wing to make more lift. so, when it is going in a turn, the left wing will make more lift than the right. this will prevent the wing from that dip in a turn with just some rudder.
keep in mind this is for a LEFT turn. if you want a right turn, just do the opposite. also know that washout alone, without the rudder input, will cause the setup i described to go right. if you think about it for a minute, that will make sense. hope this helps.