The Gurney flap (or wickerbill) is a small tab projecting from the trailing edge of a wing. Typically it is set at a right angle to the pressure-side surface of the airfoil[2] and projects 1% to 2% of the wing chord.[3] This trailing edge device can improve the performance of a simple airfoil to nearly the same level as a complex high-performance design.[4]
The device operates by increasing pressure on the pressure side, decreasing pressure on the suction side, and helping the boundary layer flow stay attached all the way to the trailing edge on the suction side of the airfoil.[5] Common applications occur in auto racing, helicopter horizontal stabilizers, and aircraft where high lift is essential, such as banner-towing airplanes.[6]
It is named for its inventor and developer, American race car driver Dan Gurney.[7][8]
These devices provided an increased region of attached flow on a wing upper surface relative to the wing without the flaps.
One candidate technology is the Gurney flap, which consists of a small plate, on the order of 1–2% of the airfoil chord in height, located at the trailing edge perpendicular to the pressure side of the airfoil.
through the proper use of Gurney flaps, the aerodynamic performance of a simple design, easy-to-build airfoil can be made practically as well as those of a modern, high performance, complex design.[permanent dead link ]
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