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A straight-winged North American FJ-1 flying next to a swept-wing FJ-2 in 1952.. There are three main reasons for sweeping a wing: [1] 1. to arrange the center of gravity of the aircraft and the aerodynamic center of the wing to coincide more closely for longitudinal balance, e.g. Messerschmitt Me 163 Komet and Messerschmitt Me 262.
It had a unique mechanism for wing sweep that combined tracks on the fuselage sides and the underside of the wings, which was actuated by hydraulically-driven ball screws positioned at the wing's inner ends. [20] The wings could be swept from 20 degrees to 70 degrees; at the 70-degree position, longitudinal control was maintained by wing tip ...
A composite photograph showing the Bell X-5’s variable-sweep wing. The Bell X-5 was the first aircraft capable of changing the sweep of its wings in flight. It was inspired by the untested wartime P.1101 design of the German Messerschmitt company. In a further development of the German design, which could only have its wing sweepback angle ...
The first successful wing sweep in flight was carried out by the Bell X-5 in the early 1950s. In the Beech Starship, only the canard foreplanes have variable sweep. Oblique wing: a single full-span wing pivots about its midpoint, as used on the NASA AD-1, so that one side sweeps back and the other side sweeps forward.
The R 1001 concept had a straight wing, but after the engineers obtained German swept wing research data, it was given a 25 degree sweep. Information on swept wings came through Switzerland and included drawings for the Messerschmitt P.1101 , P.1110 , P.1111 and P.1112 .
Full-scale prototype design of a flying test single-seat jet fighter with a wingspan of 8.06 m and a length of 8.98 m. It had a conventional tail and swept wings designed to be set at different angles while on the ground. Test flights were first intended to be undertaken with a 35-degree wing sweep, followed by a 45-degree sweep.