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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.
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 Couzinet 33 was made of wood, with a thick cantilever wing with thickness of 60 cm (24 in) at the wing roots; with no dihedral on the upper surface. The wing main-spar was continuous from wing-tip to wing-tip; and the rear spars attached to the fuselage sides.
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 ...
The Caspar C 17 was a mid-1920s German, low power, two seat ultralight aircraft with a cantilever wing of unusually high aspect ratio, flexibly attached to the fuselage to moderate gust effects. Design and development
It emerged as a mostly metal, low wing monoplane powered by a supercharged upright V-12 water-cooled engine and with a retractable conventional undercarriage. [1] [2] The cantilever wing of the Nieuport 161, as the first prototype was titled, was built in two parts around single spars with stressed skin covering and mounted with marked dihedral.
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The 161 was an all-metal monoplane with a high, semi-cantilever wing, braced on each side by a pair of parallel struts between the lower fuselage and the wing near the first outboard engine. The engines were mounted on a constant chord central section but the outer panels were tapered, [ 3 ] with ailerons interconnected to Handley Page slots ...