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Thread: C l max affected by camber of airfoil
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Old 27th Sep 2018, 00:14
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barrichello72
 
Join Date: Sep 2005
Location: italy
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Hi
mainly with reference to the trailing edge devices and to the kruger flaps as they are reaponsible for increasing the camber of the wing, amongst other things.
the slats in their extended position- b737ng - do increase the camber as well as they droop down, while in their fully extended position they allow high pressure air from the under side of the wing to flow over the top, energizing the laminar flow and thus decresing the stall speed - if i am correct.

many thanks

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