split flap

The aircraft also had split flaps, which doubled as speed brakes.

In addition there were split flaps under the trailing edges of the wing roots.

Its wing was tapered, round tipped and carried split flaps.

The rest of the trailing edge carried manually operated split flaps.

Spoilers and split flaps were eliminated at this time.

For approach and landing split flaps were fitted to the wing centre section trailing edge.

Two sets of split flaps were installed, of which either set could be selected before flight.

Wings were fitted with automatic slats and split flaps.

Inset ailerons and the split flaps were both on the outer panels.

The wing also carried trailing edge split flaps.

It was plywood covered and had split flaps inboard of the ailerons.

Metal-skinned split flaps and fixed leading edge slots were fitted.

Four position split flaps fill the trailing edges inboard of the ailerons.

The long-span ailerons were shortened and combined with centre section split flaps.

Like the Lignel 20 the 46 had somewhat inset ailerons and split flaps.

The thin wings used spruce wood spars, plywood covering and split flaps.

Split flaps are fitted as standard.

Split flaps and spoilers had also disappeared.

A pilots' union says there might have been a "split flap configuration," with one flap up and one down.

At full deflection, a split flaps acts much like a spoiler, producing lots of drag and little or no lift.

The characteristics of an airfoil with a split flap were determined in one instance, as was the effect of surface roughness.

There were pairs of split flaps inboard of the fabric covered ailerons.

It was also fitted with split flaps and had slightly enlarged rudder (similar improvements were later adapted in Junak-2).

There were split flaps on the inboard trailing edges and ailerons outboard.

The wing had automatic leading edge slats and four split flaps separated by the engine nacelles.