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- Flaps increase lift by changing the wing's camber, chord, and angle of attack12345:
- Increased camber: Flaps increase the camber of the wing, allowing it to produce more lift at slower speeds.
- Changed chord: Extending the flaps changes the shape of the wing, increasing its coefficient of lift.
- Altered angle of attack: Flaps create a bigger angle of attack on the wing, resulting in more lift.
Learn more:✕This summary was generated using AI based on multiple online sources. To view the original source information, use the "Learn more" links.Flaps increase the camber, and sometimes the area, of your wing. When you increase the camber of your wing, you also increase the amount of lift your wing can produce. With flaps down, your wing can produce more lift at slower speeds.www.boldmethod.com/learn-to-fly/aircraft-systems/…Extending the flaps changes the shape of the wing, which in turn changes its camber and chord, increasing its coefficient of lift. This allows the wing to create the same amount of lift for a given AOA. However, the higher the lift and curvature of the wing, the higher the increase in both lift-induced and parasite drag.simpleflying.com/how-aircraft-flaps-work/Flaps work by moving the trailing edge of the wing downward, which moves the chord line. Without changing the pitch of the plane, flaps create a bigger angle of attack on the wing, and therefore more lift.aerocorner.com/blog/how-flaps-work/Moving the flaps aft (toward the tail) and the slats forward increases the wing area. Pivoting the leading edge of the slat and the trailing edge of the flap downward increases the effective camber of the airfoil, which increases the lift. In addition, the large aft-projected area of the flap increases the drag of the aircraft.www.grc.nasa.gov/WWW/k-12/VirtualAero/BottleR…So flaps increase lift by changing three aspects (all found in the lift formula):
- Camber (Coefficient of Lift)
- Angle of Attack (Coefficient of Lift)
- Surface area (only certain types of flaps)
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