The effect is also used in high-lift devices such as a blown flap.

It was very advanced combination of high-lift devices in world's aviation those days.

The Series 10 was designed to have short takeoff and landing distances without the use of leading edge high-lift devices.

Furthermore, some high-lift devices increase drag during cruise.

By 1960, increases in aircraft weights required improved high-lift devices, such as variable geometry wings.

The aircraft was designed to investigate the aerodynamics of swept wings and related high-lift devices.

In aircraft design, high-lift devices are moving surfaces or stationary components intended to increase lift during certain flight conditions.

The wing will also have a clean leading edge, while having high-lift devices on the trailing edge, for good runway performance.

The wing had no high-lift devices.

Add high-lift devices to the wings.

High-lift devices, like flaps, are normally used to reduce size of the main wing, by deploying only for take off and landing.

Consumers include high-lift devices, tailplane trim, deicing, galley lift and interior services.

(High-lift devices dramatically increase lift but do so at the expense of disproportionate drag.)

During the design stage many solutions involving high-lift devices were explored including flaps blown by the "cruise" engines.

Movable high-lift devices, flaps and sometimes slats, are fitted to airfoils on almost every aircraft.

Together these high-lift devices produced a maximum wing lift coefficient of 3.0 (based on the flap-retracted wing area).

Slats are one of several high-lift devices used on airliners, such as flap systems running along the trailing edge of the wing.

The ailerons droop down to fifteen degrees with the flaps to form full-span trailing-edge high-lift devices.

The most common high-lift device is the flap, a movable portion of the wing that can be lowered into the airflow to produce extra lift.

Another common high-lift device is the slat, a small aerofoil shaped device attached just in front of the wing leading edge.

In particular, the wing arrangement with the various high-lift devices proved useful in the "hot and high" roles the VC10 would later fill.

The Model 74 was a single radial engined high-wing monoplane with trailing-edge high-lift devices for low speed and high lift performance.

The ensuing inquest principally blamed the captain for failing to maintain airspeed and configure the high-lift devices correctly.

It does not use leading-edge high-lift devices, and tracks for rear-mounted flaps are completely enclosed within the airfoil contour.

The use of high-lift devices on the leading edge of the wing lowered the landing angles to the point where the "drooping nose" was not required.