Search results
Results from the WOW.Com Content Network
The Victa Airtourer is an all-metal light low-wing monoplane touring aircraft that was developed in Australia, ... Aspect ratio: 5.65:1; Empty weight: 490 kg ...
An ASH 31 glider with very high aspect ratio (AR=33.5) and lift-to-drag ratio (L/D=56) In aeronautics, the aspect ratio of a wing is the ratio of its span to its mean chord. It is equal to the square of the wingspan divided by the wing area. Thus, a long, narrow wing has a high aspect ratio, whereas a short, wide wing has a low aspect ratio. [1]
It is a low-wing all-metal aircraft, fitted with a fixed nosewheel undercarriage and a sliding canopy. It was first certified in Japan on 6 July 1966, with certification in the United States occurring on 26 September 1967. [1] Production started in March 1968, continuing until 1986, with a total of 275 built. [2]
The Van's RV-9 and RV-9A are American two-seat, single-engine, low-wing homebuilt airplanes sold in kit form by Van's Aircraft of Aurora, Oregon. The RV-9 is the tail-wheel equipped version while the RV-9A features a nose-wheel. [4] [5] [6] The RV-9 was built around a newly designed high aspect ratio wing, featuring a Roncz airfoil.
The Spitfire wing may be classified as: "a conventional low-wing cantilever monoplane with unswept elliptical wings of moderate aspect ratio and slight dihedral".. The wing configuration or planform of a fixed-wing aircraft (including both gliders and powered aeroplanes) is its arrangement of lifting and related surfaces.
The Tecnam P2002 Sierra is a two-seat, low-wing, light aircraft. [2] A major market for the Sierra is the flight training sector; accordingly, its design and several of its major features, such as the use of a low-mounted wing and a bubble canopy, result in the aircraft being particularly well-suited to use as a trainer.
The aircraft was also to test the feasibility of low-aspect-ratio wings, and the large-scale use of titanium in aircraft structures. The design of the Douglas X-3 Stiletto is the subject of U.S. Design Patent #172,588 granted on July 13, 1954, to Frank N. Fleming and Harold T. Luskin and assigned to the Douglas Aircraft Company, Inc.
The Armstrong Whitworth AW.171 was a British project of the 1950s to develop a supersonic VTOL flying wing aircraft. It was planned to investigate the extremely low aspect ratio delta wings proposed by Professor A.A. Griffith for supersonic transports.