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Low aspect ratio: short and stubby wing. Structurally efficient, high instantaneous roll rate, low supersonic drag. Structurally efficient, high instantaneous roll rate, low supersonic drag. They tend to be used on fighter aircraft, such as the Lockheed F-104 Starfighter , and on very high-speed aircraft including the North American X-15 .
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. ... Aspect ratio: 6.34:1; Empty weight: 650 kg (1,433 lb)
Trapezoidal planform. In aeronautics, a trapezoidal wing is a straight-edged and tapered wing planform.It may have any aspect ratio and may or may not be swept. [1] [2] [3]The thin, unswept, short-span, low-aspect-ratio trapezoidal configuration offers some advantages for high-speed flight and has been used on a small number of aircraft types.
A developed version of the original V-173 prototype, the XF5U-1 was a larger aircraft. Of all-metal construction, it was almost five times heavier, with two 1,400 hp (1,193 kW) Pratt & Whitney R-2000 radial engines. The configuration was designed to create a low aspect ratio aircraft with low takeoff and landing speeds but high top speed. [2]
The Skyjacker II was designed to explore ultra-low aspect ratio wing designs and in particular the stability, controllability and capability of the configuration. The design was intended to be easily scalable to much larger aircraft. It has no complex curves and was designed to be easy to construct.
The Stout Batwing was an experimental low aspect ratio flying wing aircraft developed by William Bushnell Stout. [1] The aircraft used wood veneer construction and was an early example of cantilever wing design. The internally braced wing was also one of the first American aircraft designed without drag-producing struts.
The Be-1 featured two floats with very low aspect ratio wing sections between them and small normal wing panels extending outside the floats. Surface-piercing hydrofoils were mounted on the underside of the floats. The aircraft was powered by a single Tumansky RU-19 turbojet, mounted above the wing. The Be-1 was also equipped with landing gear.