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Control Surfaces · 04 of 04

Flaps

High-lift devices on the wing's trailing edge deployed for takeoff and landing. Flaps increase the wing's lift coefficient at a given speed — allowing slower, safer flight — but always at the cost of more drag.

What flaps do

Extending flaps increases the wing's camber (curvature) and sometimes its area. This raises the lift coefficient — meaning the wing produces more lift at the same airspeed and angle of attack. The result: the aircraft can fly slower without stalling, which is essential for approach and landing.

The cost is significantly increased drag. This drag is actually useful on approach — it allows a steeper descent angle without accelerating — but it becomes a liability if full flaps are used on takeoff, where climb performance matters more.

Quick reference

Primary effectIncreased lift coefficient; allows slower flight without stalling
Secondary effectSignificantly increased drag
LocationInboard trailing edge of each wing (between fuselage and ailerons)
Deployed forTakeoff and landing
Retracted forCruise — too much drag at cruise speed
Types of flaps: Plain flaps simply hinge down. Slotted flaps open a gap that energizes airflow over the wing, delaying separation. Fowler flaps slide aft and drop, increasing wing area as well as camber — common on airliners. Split flaps deflect only the bottom surface. Each design balances lift gain against drag penalty differently.

Slats

Slats are the leading-edge equivalent of flaps — they extend forward from the wing's leading edge to increase camber and create a slot. Most large commercial aircraft use both flaps and slats together for maximum low-speed performance on approach.

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