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Bracing may be used to resist all the various forces which occur in an airframe, including lift, weight, drag and twisting or torsion. A strut is a bracing component stiff enough to resist these forces whether they place it under compression or tension.
The drag strut member, used to transfer the load to the shear walls or frames; the chord, used to resist the tension and compression forces that develop in the diaphragm since the collector is usually incapable of handling these loads alone
A strut is a structural component commonly found in engineering, ... Throughout the 1920s and 1930s they fell out of use in favour of the low drag cantilever ...
Strut-to-wing and strut-to-fuselage junctions Strut end fairings reduce drag at these junctions. [citation needed] Tail cones Tail cones streamline the rear extremity of a fuselage by eliminating any base area which is the source of base drag. Wing root Wing roots are often faired to reduce interference drag between the wing and the fuselage.
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 ...
Strut braced monoplanes were tried but none of them were successful, not least due to the drag from the number of struts used. [ citation needed ] The structural forces acting on the spars of a biplane wing tend to be lower as they are divided between four spars rather than two, so the wing can use less material to obtain the same overall ...