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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.
In the cantilever wing, one or more strong beams, called spars, run along the span of the wing. The end fixed rigidly to the central fuselage is known as the root and the far end as the tip. In flight, the wings generate lift and the spars carry this load through to the fuselage. To resist horizontal shear stress from either drag or engine ...
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The inherent efficiency of the monoplane is best achieved in the cantilever wing, which carries all structural forces internally. However, to fly at practical speeds the wing must be made thin, which requires a heavy structure to make it strong and stiff enough. External bracing can be used to improve structural efficiency, reducing weight and ...
The Dewoitine D.33 was a single-engine low-wing cantilever monoplane of all metal construction. [4] [5] It had a slim and streamlined fuselage, the main cross section of which had been intentionally reduced to a minimum. [6]
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 aircraft was designed for a large cabin and ease-of-entry. The Sling High Wing has much parts commonality with the Sling TSi, including the cantilever wing design, with the major difference in the center section to accommodate the high-wing design. [4] [5] Cabin width is 46 in (117 cm). [5] The first flight of the prototype was in December ...
The pioneer aircraft in cantilever wings suffered from poor visibility with its top-mounted open cockpit. The follow-on aircraft, the Stout Batwing Limousine, would have a conventional fuselage and engine arrangement, and a tail mounted further aft. The all-wood cantilever wing did not need struts or braces, reducing parasitic drag on the aircraft.