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Autorotation (fixed-wing aircraft)

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During an autorotation, the upward flow of relative wind permits the main rotor blades to rotate at their normal speed. In effect, the blades are “gliding” in their rotational plane.

Autorotation is the phenomenon which results in the rotation of and lift generation by a rotorcraft's primary rotor through purely aerodynamic forces, under certain conditions. Autorotation is employed in the normal operation of an autogyro as the primary lifting mechanism, whereas it is used in helicopters only in an emergency mode after failure of the helicopter's powerplant or transmission. The autorotation of maple seeds allow them to disperse further from the tree.

Autorotation is a somewhat complex phenomenon involving the balance of opposing aerodynamic forces along the rotor's blades. Because of the rapidly varying airspeeds, Mach numbers, and angles of attack encountered by the blades as they traverse a full rotation, analysis of the aerodynamics of the rotor presents a difficult problem in fluid dynamics. Generally, however, it is the portion of the blade nearer the hub that provides the aerodynamic force (torque) tending to increase rotational speed, and the portion toward the blade tip that provides the preponderance of the lifting force. The aerodynamic drag produced by this outer blade region opposes the torque from the inner region, and thus the rotor's speed arrives at an equilibrium point at which these torques balance each other.[1] The equilibrium speed depends on a number of factors including the speed of the rotor through the air, the angle between the plane in which the blades move and the incoming air, and the collective pitch setting of the rotor.

Blade regions in vertical autorotation descent.

In helicopters, autorotation of the main rotor allows a controlled descent to an emergency landing in case of powerplant failure. Proper design of the helicopter is necessary to assure that autorotation can be usefully employed, and skilled changes to the collective and cyclic pitch are necessary during the maneuver to manage the energy of the rotor and the airspeed of the craft. Autorotation depends on the maintenance of air velocity through the rotor, and during an emergency autorotation maneuver this airspeed is provided by the helicopter's descent. In autogyros, airspeed is provided by power from an airplane-type propeller which propels the aircraft horizontally; autorotation is the sole source of rotational power for the main rotor.

Autorotation in kites

  1. Magnus-effect rotating kites that have the rotation axis bluntly normal to the stream direction use autorotation; a net lift is possible that lifts the kite and payload to altitude. The Rotoplane, the UFO rotating kite, and the Skybow rotating ribbon arch kite use the Magnus-effect resulting from the autorating wing with rotation axis normal to the stream.[2]
  2. Some kites are equipped with autorotation wings.[2]
  3. Again, a third kind of autorotation occurs in self-rotating bols, rotating parachutes, or rotating helical objects sometimes used as kite tails or kite-line laundry. This kind of autorotation drives wind and water propeller-type turbines, sometimes used to generate electricity.

See also

References