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Strut Braced Wings - Scipedia

    https://www.scipedia.com/wd/images/6/6d/Draft_Pons_Prats_410517650-4080-document.pdf
    Strut Braced Wings: the opportunities • High span Drag force is proportional to span loading and so, for a given weight, more span is beneficial • Reduced weight for a given area The ability to geometrically expand the load paths offers the possibility of reduced wing weight for a given span • Simplicity of high lift systems

Design Process: Braced Wings - KITPLANES

    https://www.kitplanes.com/design-process-braced-wings/
    A strut-braced wing consists of a main wing with internal spars braced by either a single strut or a pair of struts. The number of bracing struts depends on the internal layout of the wing itself. Strut-braced wings are a good design option for airplanes like the Zenith STOL CH 750 Super Duty, where absolute maximum cross-country performance is less important than takeoff …

Structural Optimization and Design of a Strut-Braced …

    https://vtechworks.lib.vt.edu/bitstream/handle/10919/36142/amir.pdf
    Strut-Braced Wing Aircraft Amir H. Naghshineh-Pour (ABSTRACT) A significant improvement can be achieved in the performance of transonic transport aircraft using Multidisciplinary Design Optimization (MDO) by implementing truss-braced wing concepts in combination with other advanced technologies and novel design innovations.

Conceptual Design of a Strut-Braced Wing …

    http://www.utias.utoronto.ca/wp-content/uploads/2017/09/Potter-Strut_Braced_Wing.pdf
    Why a Strut-Braced Configuration? §Optimum wing aspect ratio is a compromise between wing weight and drag §Strut-braced wing configuration allows reduced wing weight at a given aspect ratio §Allows optimization to higher aspect ratios with large reductions in induced drag §Other studies suggest 5-10% fuel burn savings compared to equivalent conventional

Wing Brackets | UNISTRUT

    https://unistrutstore.com/1-58-metal-framing/unistrut-fittings/wing-brackets.html
    Wing Shape Fittings. Unistrut Wing Shape Fittings are available in a variety of options and feature unique hole patterns for multiple Unistrut Metal Framing applications. Wing Brackets allow to you connect multiple pieces of Unistrut Channel without the need for welding. Find out how you can qualify for Free Shipping on Unistrut Wing Bracket orders over $35.

ultralight - Strut braced or wire braced airplane wings? - Aviation ...

    https://aviation.stackexchange.com/questions/54701/strut-braced-or-wire-braced-airplane-wings
    So the practical comparison is round wire vs streamline strut. A teardrop shape has 1/12th the drag of a round shape, so a round shape of 1/8" diameter has the same drag as a 1.5" thick teardrop shape. In view of that, a streamlined lift strut of say, 1" thickness (frontal area) would still have less drag than a 1/8" cable of the same length, and you only have 2 per wing vs …

Unistrut 1-5/8" Wing Shaped Channel Strut Fittings | Unistrut ...

    https://www.unistrutohio.com/wing-shaped-fittings
    Unistrut P2345 Wing Shape Fitting-1-5/8″ Channel. Unistrut P2345 Wing Shape Fitting-1-5/8″ Channel. Available in Perma-Gold by special order only. From $18.01. Unistrut P2345 Wing Shape Fitting-1-5/8″ Channel. Available in Perma-Gold by special order only.

Bracing (aeronautics) - Wikipedia

    https://en.wikipedia.org/wiki/Bracing_(aeronautics)
    Such a wing is usually also braced elsewhere, with the cabane struts forming part of the overall bracing scheme. Because cabane struts often carry engine thrust to the upper wing to overcome its drag, the loads along each diagonal between fore and aft struts are unequal and they are often formed as N-struts. They may also have cross-braced torsion wires to help stop the wing …

Strut Braced Wings Pinned (or Not) at Fuselage

    https://www.homebuiltairplanes.com/forums/threads/strut-braced-wings-pinned-or-not-at-fuselage.35148/
    To the OP: the majority of strut-braced (or wire-braced) monoplanes (e.g. Piper Cub) and biplanes (e.g. Pitts Special) use pinned joints where wing spars meet the fuselage/cabane struts. Pinned joints allow for small errors/tolerances in fabrication by only needing a handful of precision parts (e.g. strut ends).

Strut braced vs. cantilever wings - HomeBuiltAirplanes.com

    https://www.homebuiltairplanes.com/forums/threads/strut-braced-vs-cantilever-wings.11411/
    Strut braced wing weight: 108 lbs, 6 lbs spar cap, 11 lbs shear web, 5 lbs strut Other items change weight: wing attach fittings, fuselage to wing joint, control connections. I found a total weight change of 34 lbs for my design. The strut is a drag item. Large wing attach fittings can influence the fuselage and result in higher drag.

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