outer wing section in a sentence
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- British Aerospace also improved the wing by incorporating new outer wing sections.
- The outer wing section can be folded for ground transport or storage.
- To facilitate storage the outer wing sections folded to the rear for a folded span of.
- The final prototype variant was the Type D, like the Type C but with modified outer wing sections.
- Plans were also made to replace the outer wing sections and control surfaces with wooden versions to conserve aluminium.
- The outer wing sections were designed to be removable for storage, as well as being capable of carrying wing-tip tanks.
- An early example to fly, in 1940, was the Belyayev DB-LK, a twin-boom design with forward-swept outer wing sections and backwards-swept tips.
- Conversely to more conventional rear-swept wings, forward sweep geometrically creates increased angle of incidence of the outer wing sections when the wing bends under load.
- The inboard sections mate at the fuselage and the outer wing sections mate with the inboard sections approximately 12.6 feet outboard of the fuselage root chord.
- The engines, with conspicuous condensers protruding vertically from the nacelles, were mounted at the " knuckle " between the dihedral inner and the horizontal outer wing sections.
- It's difficult to see outer wing section in a sentence .
- Called " Tokyo tanks ", nine self-sealing rubber-composition tanks were mounted inside each wing on each side of the joint between the inner and outer wing sections.
- In Everett, Wash ., Boeing Commercial Airplane Group spokeswoman Kirsti Dunn said the gear involved was a " flaperon, " the movable flap on the rear of the outer wing section.
- The P-80 was a less radical design with a single British-based Allison J33 engine, with a conventional tail, but it retained a wing which was the same shape as the outer wing sections of the P-38 Lightning.
- Belalyev continued the twin boom theme with the DB-LK, which had two short fuselages either side of a very long chord wing centre section, with the outer wing sections swept forward 5 deg 42 min, tapering at 7 : 1 out to raked back tips.
- It was a simple, light design with a plywood box fuselage using the same type of engine and similar outer wing sections of the earlier single-engined aircraft . It was originally designated the DH . 84 " Dragon Moth " but marketed as the " Dragon ".
- Both types had dihedral on upper and lower outer wing sections, combined with marked anhedral in the centre section of the lower wing, a feature that optimised the view from the passenger aircraft because the wing was attached to the top of the fuselage and kept the single-wheeled undercarriage legs, mounted at the end of the centre section, short and widetrack.
- The wing centre section, between the engines, had an all-metal internal structure and the forward part of the skin was also metal, replaced by fabric further aft . The outer wing sections were slightly tapered on the leading edge only, with elliptical tips; they were entirely fabric-covered over a largely wooden structure, though the principal ribs were metal lattices . 6?of dihedral were added after the first tests.
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Last modified time: Sun, 17 Aug 2025 00:29:56 GMT
