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Aircraft wing showing the KFm3 Step. The Kline–Fogleman airfoil or KF airfoil is a simple airfoil design with single or multiple steps along the length of the wing. It was originally devised in the 1960s for paper airplanes. In the 21st century the KF airfoil has found renewed interest among hobbyist builders of radio-controlled aircraft, due ...
The KFM 107 is a two-cylinder, two-stroke, single ignition, horizontally opposed aircraft engine designed for ultralight aircraft and motor gliders. [1][2] The engine was designed and produced by the KFM (Komet Flight Motor) Aircraft Motors Division of Italian American Motor Engineering of Italy and has been out of production since 1986. [1][2]
The Rutan Model 77 Solitaire is an American, single seat, canard, mid-wing motor glider that was developed by Burt Rutan in response to the 1982 Sailplane Homebuilders Association Design Contest for a homebuilt glider. It first flew in 1982. [1] The Solitaire was declared the winner of the contest and its unusual layout attracted a great deal ...
Data from Sailplane Directory General characteristics Crew: 1 Length: 21 ft 8 in (6.604 m) Wingspan: 49 ft 3 in (15 m) Height: 5 ft 0 in (1.524 m) Wing area: 109 sq ft (10.13 m 2) Aspect ratio: 22 Airfoil: Wortmann FX 67-K-170 inboard, modified FX 67-K-150 outboard Empty weight: 535 lb (238 kg) Gross weight: 1,200 lb (544 kg) inc 483lb (220kg) water ballast Performance Maximum speed: 133 kn ...
The Monnett Moni is a sport aircraft developed in the United States in the early 1980s and marketed for homebuilding. Designed by John Monnett, who coined the term "air recreation vehicle" to describe it, [1] it is a single-seat motorglider with a low, cantilever wing and a V-tail. Construction is of metal throughout, and it is intended to be ...
The GW-2 also uses a V-tail. [1] [2] [3] The GW-2 is an all-metal design, with doped aircraft fabric covering on the aft part of the wing, behind the spar. The wing mounts spoilers for glide-path control. The landing gear is a fixed monowheel, with a secondary skid. [1] [2] The prototype GW-2 was registered as N94291 and first flown in 1964.
Garner, Christian (2016), "An Unfulfilled Promise: The U.S. Glider Pilot Training Program and Lamesa Field, Texas, During World War II." Military History of the West 45 (June 2016): 46–76. Shaw, Frederick J. (2004), Locating Air Force Base Sites History's Legacy, Air Force History and Museums Program, United States Air Force, Washington DC, 2004.
The high aspect ratio wing also made the Lazair a good glider, giving it a 12:1 glide ratio, and it could be soared in even light thermal conditions. [ 7 ] [ 8 ] The wing structure comprises an aluminum "D" cell leading edge , foam ribs and an aluminum tubular trailing edge .
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