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  2. Sikorsky S-69 - Wikipedia

    en.wikipedia.org/wiki/Sikorsky_S-69

    The Advancing Blade Concept system consisted of two rigid, contra-rotating rotors (30 inches apart) [9] which made use of the aerodynamic lift of the advancing blades. At high speeds, the retreating blades were offloaded, as most of the load was supported by the advancing blades of both rotors and the penalty due to stall of the retreating ...

  3. Dissymmetry of lift - Wikipedia

    en.wikipedia.org/wiki/Dissymmetry_of_lift

    [1]: 2–14 Rotor blades are designed to flap: the advancing blade flaps up and develops a smaller angle of attack due to a change in relative wind vectors, thus producing less lift than a rigid blade would. Conversely, the retreating blade flaps down, develops a higher angle of attack due to a change in relative wind vectors, and generates ...

  4. Dragonfly (Titan space probe) - Wikipedia

    en.wikipedia.org/wiki/Dragonfly_(Titan_space_probe)

    Dragonfly is designed as a rotorcraft lander, much like a large quadcopter with double rotors, which is known as an octocopter. [3] The rotor configuration provides redundancy to enable the mission to tolerate the loss of at least one rotor or motor. [3] Each of the craft's eight rotors is 1.35 m (4.4 ft) in diameter.

  5. After damaging a rotor blade, NASA’s Ingenuity helicopter ...

    www.aol.com/news/history-making-martian...

    Perseverance captured an image of Ingenuity on August 2, 2023, the day before the helicopter's 54th flight. - NASA/JPL-Caltech

  6. Dynamic stall on helicopter rotors - Wikipedia

    en.wikipedia.org/wiki/Dynamic_stall_on...

    Rotor map of dynamic stall locations for all conditions. Stage 4: full separation of the flow on the upper surface of the airfoil can be observed, accompanied by the peak of nose-down pitch moment. Stage 5: the full flow reattachment is achieved as the AoA gradually decreases until it is fairly smaller than the static stall angle. [10]

  7. Slowed rotor - Wikipedia

    en.wikipedia.org/wiki/Slowed_rotor

    The McDonnell XV-1 could slow its rotor from 410 to 180 RPM. The slowed rotor principle is used in the design of some helicopters.On a conventional helicopter the rotational speed of the rotor is constant; reducing it at lower flight speeds can reduce fuel consumption and enable the aircraft to fly more economically.

  8. Coaxial-rotor aircraft - Wikipedia

    en.wikipedia.org/wiki/Coaxial-rotor_aircraft

    A coaxial-rotor aircraft is an aircraft whose rotors are mounted one above the other on concentric shafts, with the same axis of rotation, but turning in opposite directions (contra-rotating). This rotor configuration is a feature of helicopters produced by the Russian Kamov helicopter design bureau.

  9. Bell XV-15 - Wikipedia

    en.wikipedia.org/wiki/Bell_XV-15

    It continued in primarily NASA test operations until September 2003. The shortest takeoff distance was achieved with the nacelles at 75 degrees angle. [8] After N703NA was retired from test operations, it was donated to the Smithsonian National Air and Space Museum in Washington, D.C. The XV-15 was flown cross-country from Fort Worth, Texas to ...