Slats are used to reconfigure the wing in a high speed, or high angle-of-attack maneuover. When the units of angle of attack increase, the wing chord decreases. Slats compensate for this occurance.
It depends on the general construction of the aircraft. Commonly used material are: aluminum, wood, cloth, and fiberglass. BTW, what are slats??
Lift can be increased by curving the wing downward. Most aircraft have 'flaps' at the rear inner edge of the wing to achieve this. Some aircraft even have 'slats' at the front of the wing to increase lift even more. - If you google 'aircraft slats', you will see a great picture of slats and flaps on an Airbus A310
Slats and flaps increase drag and also increaselift. The increase in drag slows the aircraft down, and the increase in lift lowers the stall speed, which slows the landing speed of the aircraft.
There are numerous parts on an aircraft. Each one has a specific purpose. Turbine engines generate the thrust while the wings generate lift. Other parts include the cockpit, fuselage, and slats.
The function of flaps and slats on a plane are simple but important. While landing and taking off the flaps are down so the plane lift increase and the plane can maintain flight with lower air speeds. While cruse altitude flaps are in to reduce drag, safe fuel and the chance to speed up.
To "propel" the aircraft through the air.
1. Ailerons for Bank 2. Elevator for Pitch 3. Rudder for Yaw 4. Flaps for added lift (Also Slats, in front of the Wing on some aircraft)
Slats on a plane are aerodynamic devices attached to the leading edge of the wings. They extend and increase the wing's curvature, enhancing lift at lower speeds, particularly during takeoff and landing. By improving airflow over the wings, slats help prevent stalling and allow the aircraft to maintain better control during critical phases of flight.
The Wilga is a very unique STOL aircraft which can land and take off in very short distances. The leading edge slats and the unique wing design of this aircraft enable it to fly as slow as 35 knots, and the aircraft will not stall. For pictures go to http://www.thaiflyingclub.com/linkwilga.html
Airplanes use a combination of slats and flaps in order to increase lift and increase drag. The slats are located on the leading edge of the wing and the flaps on the trailing edge. Flaps and slats when extended forward and aft increase the wing area which increases lift. When the flaps and slats are further extended they curve downwards increasing the camber of the wing which also increases lift. The greater the lift, the greater the drag. Deploy the flaps a little and lift overcomes the drag, fully extend them and the drag overcomes the lift. For takeoff the flaps and slats may be extended just a few degrees to increase lift. When flaps and slats are fully deployed in landing configuration, the lift is great but so is the drag and this in turn helps to slow down the airplane on decent to land.
In order to designate components by their position on the aircraft, the general rule of thumb is to number them from Left(or Port) to Right(Starboard). This is true for Engines, flaps, slats. This usually does not apply to Fuel Tanks which are usually designated by Left Outboard or Right Inboard, etc.
Slats Long died in 1964.