In aviation, a strake is an aerodynamic surface generally mounted on the fuselage of an aircraft to improve the flight characteristics either by controlling the airflow (acting as large vortex generators) or by simple stabilising effect.
Leading edge root extensions (LERX) are also sometimes referred to as wing strakes.
On both supersonic and subsonic types, smaller strakes are sometimes applied to the forward fuselage to control the fuselage flow at high angles of attack ; for example the Concorde SST has small nose strakes "to get a better directional stability".
For wing strakes, see Leading edge root extension (LERX).
Double delta wing aircraft (Concorde, Tupolev Tu-144, Boeing 2707 SST project) featured a forward extended leading edge that may be considered as a wing strake ; it provides the same additional vortex lift at high AoA by leading edge suction.
One or two ventral strakes are sometimes positioned under the fuselage, as large vortex generators, to provide a better tail surfaces efficiency. Typical examples can be seen on the SOCATA TB family or the Lockheed F-104 Starfighter.
Rear strakes - tail fins
One or two large fins or strakes are sometimes positioned under the rear fuselage or below the empennage, to provide adequate stability at high angles of attack when the tail fin is shielded from the main airstream by the fuselage and/or the wing wake. Typical examples can be seen on the Piaggio P.180 Avanti, Learjet 60 and Beechcraft 1900D.
The Grumman X-29 research aircraft had rear fuselage lateral fins or "Tail fins", sometimes called strakes, continuous with the trailing edge of the main wing. This allowed the positioning of a rear control surface at the end of each fin. Together with the main and forward (canard) wing control surfaces, this effectively gave it a three-surface configuration.
Anti-spin leading edge strakes, or spin strakes, or antispin fillet  may be placed at the tailplane roots of generally aerobatic aircraft, such as the de Havilland Tiger Moth (British version), Scottish Aviation Bulldog, de Havilland Canada DHC-1 Chipmunk. Ventral or dorsal fins increasing the directional stability are also used used as anti-spin devices.
A dorsal fin is a triangular strake extending from the top of the fuselage to the leading edge of the vertical fin. Dorsal fins are used to increase the directional stability at high yaw angles and delay the vertical tail stall. "Although they do not have any effect within the range of +/- 3° of yaw, between 10° and 50° the stabilising influence of the fins is considerable".
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Certain air-deployed munitions, particularly "dumb" or unguided 500-pound bombs, are often retrofitted with bolt-on strake sets. Designed as an open collar with strakes fitted to the outside face, these strake sets are used to alter and normalize the aerodynamics of the weapon, yielding greater accuracy. As most such munitions were manufactured with only tail-mounted stabilizer fins, the addition of longitudinal strakes proves a much cleaner flow of air around the weapon during its glide, reducing the tendency to yaw and improving terminal accuracy.
Strakes are also often found on "smart" or guided munitions as an aid to the guidance system. By stabilizing the slipstream of air traveling over the weapon, the actions of control surfaces are much more predictable and precise, again improving the accuracy of the weapon.
- André Peyrat-Armandy, Les avions de transport modernes et futurs, Teknea, 1997, p. 229
- Hoerner, Fluid Dynamic Lift, Double Delta Wings
- In Hoerner Fluid Dynamic Lift, "Tail fins - Dorsal and others fins on fuselage"
- Miller, J.; The X-Planes, 2nd Printing, Speciality Press (1985)
- Nasa TN D-6575, Summary of spin technology as related to the light general-aviation airplanes, fig. 10
- Daroll Stinton, The design of the aeroplane, Lateral an directional stability and spinning, p.461.
- Hoerner, Fluid Dynamic Lift, "A device expected to improve the directional characteristics are dorsal and/or ventral fins".
- Hoerner, Fluid Dynamic Lift, 13-23, Dorsal Fins