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  2. File:Active Aeroelastic Wing time lapse.ogv - Wikipedia

    en.wikipedia.org/wiki/File:Active_Aeroelastic...

    This is Video (Ogg Theora) This 53 second movie clip shows a time lapsed film of Active Aeroelastic Wing (AAW) Wing Loads Test Active Aeroelastic Wing is a two-phase NASA--Air Force flight research program to investigate the potential of aerodynamically twisting flexible wings to improve maneuverability of high-performance aircraft at transonic and supersonic speeds, with traditional control ...

  3. Wing twist - Wikipedia

    en.wikipedia.org/wiki/Wing_twist

    Wing twist is an aerodynamic feature added to aircraft wings to adjust lift distribution along the wing.. Often, the purpose of lift redistribution is to ensure that the wing tip is the last part of the wing surface to stall, for example when executing a roll or steep climb; it involves twisting the wingtip a small amount downwards in relation to the rest of the wing.

  4. Wing warping - Wikipedia

    en.wikipedia.org/wiki/Wing_warping

    This was a significant influence on early aircraft designers. The Wright brothers were the first group to use warping wings. Their first plane mimicked the bird's flight patterns and wing form. [3] In practice, since most wing warping designs involved flexing of structural members, they were difficult to control and liable to cause structural ...

  5. Boeing X-53 Active Aeroelastic Wing - Wikipedia

    en.wikipedia.org/wiki/Boeing_X-53_Active_Aero...

    The X-53 Active Aeroelastic Wing (AAW) development program is a completed American research project that was undertaken jointly by the Air Force Research Laboratory (AFRL), Boeing Phantom Works and NASA's Dryden Flight Research Center, where the technology was flight tested on a modified McDonnell Douglas F/A-18 Hornet.

  6. Flight control surfaces - Wikipedia

    en.wikipedia.org/wiki/Flight_control_surfaces

    After a few seconds the aircraft will tend to bank in the direction of yaw. This arises initially from the increased speed of the wing opposite to the direction of yaw and the reduced speed of the other wing. The faster wing generates more lift and so rises, while the other wing tends to go down because of generating less lift.

  7. Aeroelasticity - Wikipedia

    en.wikipedia.org/wiki/Aeroelasticity

    Divergence is a phenomenon in which the elastic twist of the wing suddenly becomes theoretically infinite, typically causing the wing to fail. Control reversal is a phenomenon occurring only in wings with ailerons or other control surfaces, in which these control surfaces reverse their usual functionality (e.g., the rolling direction associated ...

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  9. Aerobatic maneuver - Wikipedia

    en.wikipedia.org/wiki/Aerobatic_maneuver

    A spin is more complex, involving intentionally stalling a single wing, causing the plane to descend spiraling around its yaw axis in a corkscrew motion. A hammerhead (also known as a stall turn ) is performed by pulling the aircraft up until it is pointing straight up (much like the beginning of a loop), but the pilot continues to fly straight ...