page_title: Leading-edge slot
section_title: Operation
hierarchical_section_title: Leading-edge slot / Operation
caption_attribution_description: English: A Canadian Stinson 108-3 (C-FSKK) with gear adaptation for snow. The partial span leading edge slot is visible. I took this photo and release it to the public domain
context_page_description: A leading-edge slot is a fixed aerodynamic feature of the wing of some aircraft to reduce the stall speed and promote good low-speed handling qualities. A leading-edge slot is a spanwise gap in each wing, allowing air to flow from below the wing to its upper surface. In this manner they allow flight at higher angles of attack and thus reduce the stall speed.
context_section_description: A leading-edge slot is a fixed (non-closing) gap behind the wing's leading edge.  Air from below the wing can accelerate through the slot towards the low pressure region above the wing, and exit from the slot moving parallel to the upper wing surface.  This high-speed flow then mixes with the boundary layer attached to the upper surface and delays boundary layer separation from the upper surface.
  Slots naturally exact a penalty on the aircraft in which they are used. This is because they contribute to drag compared to an unslotted wing.  The extra drag at low speed is acceptable because of the beneficial reduction in stall speed and improvement in handling characteristics, but at higher speeds the extra drag contributed by slots is a significant disadvantage because it reduces cruising speed and increases fuel consumption per unit distance flown.
  One way to reduce the cruise drag of slots is to make them able to be closed. This arrangement is known as leading-edge slats.  Aerodynamically, slats work in the same way as fixed slots but slats can be retracted at higher speeds when they are not needed. Slats, in turn, are heavier and more complex than slots.
  At low angles of attack the airflow through the slot is insignificant, although it contributes to drag.  At progressively higher angles of attack, the flow of air through the slot becomes increasingly significant, accelerating from the higher pressure region below the wing to the lower pressure region on top of the wing.   At high angles of attack the fastest airspeed relative to the airfoil is very close to the leading edge, on the upper surface.  In this region of high local airspeed, skin friction (viscous force) is very high and the boundary layer arriving at the slot on the upper wing has lost much of its total pressure (or total mechanical energy) due to this friction.  In contrast, the air passing through the slot has not experienced this high local airspeed or high skin friction, and its total pressure remains close to the free-stream value.  The mixing of the upper surface boundary layer with air arriving through the slot re-energises the boundary layer which then remains attached to the upper surface of the wing to a higher angle of attack than if the slot were not there.  The leading-edge slot was therefore one of the earliest forms of boundary layer control.
caption: Partial-span leading-edge slot in the wing of a Stinson 108-3
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