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Flap (Aircraft)
CHF 37.35
Auf Lager
SKU
7IRE0J8U582
1 Verfügbar 
Geliefert zwischen Mi., 21.01.2026 und Do., 22.01.2026
Details
Flaps are hinged surfaces on the trailing edge of the wings of a fixed-wing aircraft. As flaps are extended, the stalling speed of the aircraft is reduced, which means that the aircraft can fly safely at slower speeds (especially during take off and landing). Flaps are also used on the leading edge of the wings of some high-speed jet aircraft, where they may be called Krueger flaps. Extending flaps increases the camber of the wing airfoil, thus raising the maximum lift coefficient. This increase in maximum lift coefficient allows the aircraft to generate a given amount of lift with a slower speed. Therefore, extending the flaps will reduce the stalling speed of the aircraft. Extending flaps also increases drag. This can be beneficial in the approach and landing phase because it helps to slow the aircraft. Another useful side-effect of flap deployment is a decrease in aircraft pitch angle. This provides the pilot with a greater view over the nose of the aircraft and allows a better view of the runway during approach and landing. Some trailing edge flap systems increase the planform area of the wing in addition to changing the camber.
Weitere Informationen
- Allgemeine Informationen
- GTIN 09786130674908
- Editor Frederic P. Miller, Agnes F. Vandome, John McBrewster
- Sprache Englisch
- Genre Technik
- Anzahl Seiten 72
- Größe H220mm x B150mm x T4mm
- Jahr 2010
- EAN 9786130674908
- Format Fachbuch
- ISBN 978-613-0-67490-8
- Titel Flap (Aircraft)
- Untertitel Wing, Fixed-wing aircraft, Stall (flight), Krueger flaps, Camber (aerodynamics), Lift coefficient, Drag (physics), Planform, True airspeed, Drag coefficient, Takeoff, Flight controls, Aileron
- Gewicht 125g
- Herausgeber Alphascript Publishing
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