Both wings also had leading edge slots along their full length.

Among the notable differences were the introduction of leading edge slots.

Some airplanes have been designed with fixed leading edge slots.

Its working principle can be compared to a leading edge slot on an aircraft wing.

The design initially featured both Flap (aircraft) and a leading edge slot.

Leading edge slots are fitted ahead of the ailerons.

Ailerons were only fitted to the upper wing, which also had leading edge slots.

The wing was fitted with leading edge slots and flaps to give a good landing performance.

The wing is equipped with leading edge slots.

Both types carried ailerons and leading edge slots on the upper wing only.

The leading edge slot was therefore one of the earliest forms of boundary layer control.

This wing had full span leading edge slots and camber changing flaps.

A fixed leading edge slot can increase the maximum lift coefficient of an airfoil section by 40%.

Leading edge slot, an aerodynamic device used on fixed wing aircraft

The outer panels carried both ailerons and built-in leading edge slots with no moving parts.

The wooden wings include leading edge slots.

Trailing edge flaps and leading edge slots were interconnected.

The wings were fitted with trailing edge flaps and fixed leading edge slots.

One off (c/n 163) with metal hull and Handley-Page leading edge slots.

The stabilizers also had the Handley-Page leading edge slots installed on the inboard side.

The six Hendons were used for extensive trials to investigate various configurations of leading edge slots/slats.

It was the first German commercial aircraft to incorporate leading edge slots and trailing edge flaps.

Modification of such an airfoil with a fixed leading edge slot can increase the stalling angle to between 22 and 25 .

Other than ailerons, the simple wing does not use flaps, leading edge slots or any other lift devices.

There were fixed leading edge slots and trailing edge ailerons but no conventional flaps.