In the aerospace context, a flap is a type of high-lift device used to increase the lift of an aircraft's wing at a given airspeed.
Flaps are usually located on the trailing edge of the wing and can be extended downward to increase the camber, or curvature, of the wing. This increases the lift generated by the wing and allows the aircraft to take off and land at lower speeds.
There are several types of flaps, including plain flaps, split flaps, slotted flaps, and fowler flaps. Each type of flap works by deflecting the airflow over the wing in a specific way, which changes the pressure distribution across the wing and increases lift.
Here are some examples of how flaps are used in different types of aircraft:
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In a small single-engine airplane flaps may be used to slow the aircraft down during the landing approach and to increase lift during takeoff.
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In a large commercial jetliner, flaps may be extended to their maximum setting during takeoff to provide extra lift, and then retracted once the aircraft is at cruising altitude to reduce drag.
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In a military fighter jet, flaps may be used to increase lift and maneuverability during combat operations.
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In a helicopter, flaps called "cyclic flaps" may be used to change the pitch and direction of the rotor blades, allowing the helicopter to hover, move forward, or move backward.
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Plain flap: This is the simplest type of flap, which is hinged at the rear edge of the wing and moves downwards to increase the wing's camber.
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Split flap: This type of flap is similar to the plain flap, but it is hinged at the front edge of the flap, causing it to split open to the rear. Split flaps are less effective than plain flaps, but they are simpler and less expensive to manufacture.
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Fowler flap: This is a complex type of flap that moves backwards and downwards to increase the wing's area and camber. Fowler flaps are commonly used on large commercial airliners to allow for slower landing speeds and shorter takeoff runs.
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Slotted flap: This type of flap is designed with a slot between the flap and the wing, which allows high-pressure air to flow from the bottom of the wing to the top, increasing the lift and reducing drag.
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Krueger flap: This is a specialized type of flap that is located on the leading edge of the wing, and is used to increase lift at low speeds. Krueger flaps are commonly used on large commercial airliners, and are particularly effective at reducing the stall speed of the aircraft.
In addition to flaps, there are several other devices used in aerospace engineering to control the lift and drag of an aircraft. These include:
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Ailerons: These are hinged surfaces on the trailing edge of the wing that are used to control the roll of the aircraft.
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Elevators: These are hinged surfaces on the trailing edge of the horizontal stabilizer that are used to control the pitch of the aircraft.
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Rudder: This is a hinged surface on the trailing edge of the vertical stabilizer that is used to control the yaw of the aircraft.
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Spoiler: This is a device used to reduce the lift generated by the wing, typically by disrupting the airflow over the upper surface of the wing.
Overall, flaps and other control devices are critical components of modern aircraft, allowing pilots to safely take off and land at lower speeds, and providing the ability to control the aircraft's movement in all three dimensions. By understanding the design and function of these devices, aerospace engineers are able to develop more efficient and effective aircraft designs that are safer and more reliable for passengers and crew.
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