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In aeronautics, bracing comprises additional structural members which stiffen the functional airframe to give it rigidity and strength under load. Bracing may be applied both internally and externally, and may take the form of struts, which act in compression or tension as the need arises, and/or wires, which act only in tension.
Most aircraft bracing struts are principally loaded in compression, with wires taking the tension loads. Lift struts came into increasing use during the changeover period and remain in use on smaller aircraft today where ultimate performance is not an issue. Typically, they are applied to a high wing monoplane and act in tension during flight.
It will use an extra-long and thin wing design stabilized by diagonal bracing struts, which is known as a Transonic Truss-Braced Wing. The aircraft configuration is based on research studies referred to as "Subsonic Ultra-Green Aircraft Reach (SUGAR)" which extensively studied truss-bracing and hybrid electric technologies. [1] [2]
The ALPHA STRUT is suitable for a variety of aircraft and other aerospace medium to high load bearing applications, including primary and secondary aircraft structures, tie rods, push/pull control ...
The UFAG C.I incorporated the best features of the Brandenburg C.II(U) with single-bay wings and 'I' strut inter-plane bracing, which was replaced wing conventional steel-tube interplane struts in production aircraft.
Strut braced: one or more stiff struts help to support the wing, as on the Fokker D.VII. A strut may act in compression or tension at different points in the flight regime. Wire braced: alone (as on the Boeing P-26 Peashooter) or, more usually, in addition to struts, tension wires also help to support the wing. Unlike a strut, a wire can act ...
The fuselage of the D.I was used as a basis and the two aircraft shared the same basic structural elements of longerons and formers covered by plywood. [2] Steel was used extensively in the structure of the tail unit, such as bracing struts and the framework of both the elevator and rudder.
The straight-wing Reliant has a wing of constant chord and thickness which is supported by two struts each side with additional bracing struts. In contrast the taper-wing Reliant has the broadest chord and thickness of the wing at mid-span, with the outer wing trailing edge heavily angled forward and a rounded cutout on the leading edge root ...
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