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Other varieties of flaps could also be geared up with a number
of slots to extend their effectiveness, a typical
setup on many modern airliners. Leading edge slats and slots are mounted on the top of the wings' leading
edge and whereas they may be both mounted or retractable, when deployed
they supply a slot or hole underneath the slat to force
air towards the highest of the wing, which is absent on a Krueger flap.
I handed one which looked as if it was hanging motionless within the air (I am too fast!).
In principle, if 80% of wing is laminar, then overall drag could possibly be reduced by 25%.
The frictional pressure between the air and the aircraft floor, often called viscous drag, is far larger in a
turbulent boundary layer than in a laminar one. The principal type of energetic laminar-flow
management is removal of a small amount of the boundary-layer air
by suction through porous supplies, multiple slender floor slots,
or small perforations (boundary layer suction). The Northrop X-21A was an experimental aircraft designed to test wings with laminar circulation control.
When installed on the wings they differ from flaps and
spoilers in that they aren't supposed to change the raise and are constructed strongly enough to be deployed at a lot
greater speeds.
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