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From Wikipedia, the free encyclopedia

A twin-tailed B-25 Mitchell in flight

A twin tail is a type of vertical stabilizer arrangement found on the empennage of some aircraft. Two vertical stabilizers—often smaller on their own than a single conventional tail would be—are mounted at the outside of the aircraft's horizontal stabilizer. This arrangement is also known as an H-tail,[1] as it resembles a capital "H" when viewed from the rear. The twin tail was used on a wide variety of World War II multi-engine designs that saw mass production, especially on the American B-24 Liberator and B-25 Mitchell bombers, the British Avro Lancaster and Handley Page Halifax heavy bombers, and the Soviet Union's Petlyakov Pe-2 attack bomber.

It can be easily confused for the similarly named twin-boom (or "double tail") arrangement, which has two separate tail-booms from the same fuselage rather than a single tail with twin stabilizers (a singular "twin tail" vs. two identical tails).

One variation on the twin tail is the triple tail, but the twin-boom arrangement can also be considered a variation of the twin tail.

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Transcription

Design

Twin tail of an Avro Lancaster
The twin tail of a Chrislea Super Ace, built in 1948
High-mounted twin tail of a Blackburn Beverley transport
Twin tail of a Textron AirLand Scorpion ISR aircraft

Separating the control surfaces allows for additional rudder area or vertical surface without requiring a massive single tail. On multi-engine propeller designs twin fin and rudders operating in the propeller slipstream give greater rudder authority and improved control at low airspeeds, and when taxiing. A twin tail can also simplify hangar requirements, give dorsal gunners enhanced firing area, and in some cases reduce the aircraft's weight.[2][failed verification] It also affords a degree of redundancy: if one tail is damaged, the other may remain functional.

Most often, the twin vertical surfaces are attached to the ends of the horizontal stabilizer, but a few aircraft, like the Armstrong Whitworth Whitley, Mitsubishi G3M and Dornier Do 19 bombers, had their twin vertical surfaces mounted to the upper surface of the fixed stabilizer instead, at some distance inwards from the horizontal stabilizer's tips.

Variations

Many canard aircraft designs incorporate twin tails on the tips of the main wing. Very occasionally, three or more tails are used, as on the Breguet Deux-Ponts, Lockheed Constellation and Boeing 314 Clipper. A very unusual design can be seen on the C-2 Greyhound and E-2 Hawkeye, which has two additional vertical tails fixed to the horizontal stabilizer between the normal vertical twin-tail surfaces. This arrangement was chosen for the stringent size limitations of carrier-based aircraft.

A special case of twin tail is the twin-boom tail or double tail, where the aft airframe consists of two separate fuselages, "tail booms", which each have a rudder but are usually connected by a single horizontal stabilizer. Examples of this construction are the twin-engined Lockheed P-38 Lightning; Northrop P-61 Black Widow; Focke-Wulf Fw 189; the single jet-engined de Havilland Vampire; cargo-carrying Fairchild C-119 Flying Boxcar and the little known Transavia PL-12 Airtruk.

Notable twin-tail aircraft

Significant aircraft with twin tails include the Consolidated B-24 Liberator, Handley Page Halifax, Avro Lancaster, and P-38 Lightning. The arrangement is not limited to World War II-era aircraft, however. Many fighter aircraft, like the Grumman F-14 Tomcat, McDonnell Douglas F-15 Eagle, Sukhoi Su-27, MiG-29, and Fairchild Republic A-10 Thunderbolt II, make use of twin tail configurations, as do civilian and cargo designs like the Antonov An-14, Antonov An-22, Antonov An-28, Antonov An-38, Antonov An-225, Beechcraft 18, Beriev Be-12, ERCO Ercoupe, Short 330, Rutan Long-EZ and SpaceShipOne.

The V-22 Osprey uses a twin tail arrangement.

See also

References

  1. ^ Schiff, Barry: Flying, page 15. Golden Press, New York, 1971. Library of Congress 78-103424
  2. ^ Pilot Training Manual for the B-25 Mitchell Bomber. Headquarters, AAF, Office of Flying Safety. 1944. p. 17. Retrieved 7 May 2021. A twin tail section with large rudders increases stability and manuverability and allows a greater concentration of firepower to the rear.
This page was last edited on 19 April 2024, at 15:49
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