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  2. Slip (aerodynamics) - Wikipedia

    en.wikipedia.org/wiki/Slip_(aerodynamics)

    Sideslip causes one main landing gear to touch down first, followed by the second main gear. This allows the wheels to be constantly aligned with the track, thus avoiding any side load at touchdown. The sideslip method for crosswind landings is not suitable for long-winged and low-sitting aircraft such as gliders , where instead a crab angle ...

  3. Vertical stabilizer - Wikipedia

    en.wikipedia.org/wiki/Vertical_stabilizer

    The vertical stabilizer is the fixed vertical surface of the empennage. A vertical stabilizer or tail fin [1] [2] is the static part of the vertical tail of an aircraft. [1] The term is commonly applied to the assembly of both this fixed surface and one or more movable rudders hinged to it.

  4. Turn and slip indicator - Wikipedia

    en.wikipedia.org/wiki/Turn_and_slip_indicator

    Intentionally putting an aircraft into a slip is used as a forward slip and a sideslip. These slips are performed by applying opposite inputs of the aileron and rudder controls. A forward slip allows a pilot to quickly drop altitude without gaining unnecessary speed, while a sideslip is one method utilized to perform a crosswind landing.

  5. AAR Corp - Wikipedia

    en.wikipedia.org/wiki/AAR_Corp

    In 2017, AAR was chosen as the prime contractor for a 15-year, $909 million landing gear award to provide total supply-chain management to support all U.S. Air Force and contractor requisitions received for all C-130, KC-135 & E-3 landing gear parts.

  6. Spoiler (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Spoiler_(aeronautics)

    The inner workings of spoilers in lift dump deployment during the landing of an Airbus A320 A spoiler (the parts of the wing that are raised up) during the landing of an Airbus A321 The right wing of a Boeing 767-300ER during descent with spoilers partially deployed Spoilers deployed to slow down for descent on a Qantas Boeing 737-800

  7. Dihedral (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Dihedral_(aeronautics)

    Dihedral effect is defined simply to be the rolling moment caused by sideslip and nothing else. Rolling moments caused by other things that may be related to sideslip have different names. Dihedral effect is not caused by yaw rate, nor by the rate of sideslip change. Since dihedral effect is noticed by pilots when "rudder is applied", many ...

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    www.aol.com/lifestyle/walmart-holiday-deals-2024...

    Amazon's October Prime Day sale might be over, but Walmart's Holiday Deals event is still going strong for several more days with brand new, hot-off-the-press deals unveiling now through through ...

  9. Aircraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_dynamics

    An aircraft is streamlined from nose to tail to reduce drag making it advantageous to keep the sideslip angle near zero, though an aircraft may be deliberately "sideslipped" to increase drag and descent rate during landing, to keep aircraft heading same as runway heading during cross-wind landings and during flight with asymmetric power.

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