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  2. Skyworks Aeronautics - Wikipedia

    en.wikipedia.org/wiki/Skyworks_Aeronautics

    The company discontinued Sparrowhawk kit production, but formed American Autogyro, as a subsidiary to produce and sell Sparrowhawk kits as a separate business. In November, 2005, the U.S. Defense Advanced Research Projects Agency (DARPA) selected a company-led team to design a proof-of-concept high-speed, long-range, VTOL GBA-DARPA Heliplane ...

  3. Rotor wing - Wikipedia

    en.wikipedia.org/wiki/Rotor_wing

    The various types of such rotor wings may be classified according to the axis of the rotor. Types include: [1] [2] Vertical-axis. Conventional rotary wings as used by modern rotorcraft. Spanwise horizontal-axis. Wing rotor: an airfoil-section horizontal-axis rotor which creates the primary lift. Magnus rotor: a rotor which creates lift via the ...

  4. Rotorwing-Aero - Wikipedia

    en.wikipedia.org/wiki/Rotorwing-Aero

    Rotorwing-Aero was an American aircraft design firm founded in the 1980s by Monte Hoskins and based in Salt Lake City, Utah.The company specialized in the design of autogyros in the form of plans for amateur construction for the US FAR 103 Ultralight Vehicles rules.

  5. Rotorcraft - Wikipedia

    en.wikipedia.org/wiki/Rotorcraft

    An early American proposal was the conversion of the Lockheed F-104 Starfighter with a triangular rotor wing. The idea was later revisited by Hughes. [4] The Sikorsky S-72 research aircraft underwent extensive flight testing. In 1986 the Sikorsky S-72 Rotor Systems Research Aircraft (RSRA) was fitted with a four-bladed stopped rotor, known as ...

  6. Cyclogyro - Wikipedia

    en.wikipedia.org/wiki/Cyclogyro

    The cyclogyro wing resembles a paddle wheel, with airfoil blades replacing the paddles. Like a helicopter, the blade pitch (angle of attack) can be adjusted either collectively all together or cyclically as they move around the rotor's axis. In normal forward flight, the blades are given a slight positive pitch at the upper and forward portions ...

  7. Disk loading - Wikipedia

    en.wikipedia.org/wiki/Disk_loading

    This energy transfer from the rotor to the air is the induced power loss of the rotary wing, which is analogous to the lift-induced drag of a fixed-wing aircraft. Conservation of linear momentum relates the induced velocity downstream in the far wake field to the rotor thrust per unit of mass flow .