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  2. Category:Aircraft wing components - Wikipedia

    en.wikipedia.org/wiki/Category:Aircraft_wing...

    Pages in category "Aircraft wing components" The following 28 pages are in this category, out of 28 total. This list may not reflect recent changes. A.

  3. Spar (aeronautics) - Wikipedia

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

    The Junkers all-metal corrugated-covered wing / multiple tubular wing spar design format was emulated after World War I by American aviation designer William Stout for his 1920s-era Ford Trimotor airliner series, and by Russian aerospace designer Andrei Tupolev for such aircraft as his Tupolev ANT-2 of 1922, upwards in size to the then-gigantic ...

  4. Airplane - Wikipedia

    en.wikipedia.org/wiki/Airplane

    An airplane (North American English) or aeroplane (British English), informally plane, is a fixed-wing aircraft that is propelled forward by thrust from a jet engine, propeller, or rocket engine. [1] Airplanes come in a variety of sizes, shapes, and wing configurations .

  5. Wing configuration - Wikipedia

    en.wikipedia.org/wiki/Wing_configuration

    A fixed-wing aircraft may have more than one wing plane, stacked one above another: Biplane: two wing planes of similar size, stacked one above the other. The biplane is inherently lighter and stronger than a monoplane and was the most common configuration until the 1930s. The very first Wright Flyer I was a biplane.

  6. Leading-edge slat - Wikipedia

    en.wikipedia.org/wiki/Leading-edge_slat

    Slats are high-lift devices typically used on aircraft intended to operate within a wide range of speeds. Trailing-edge flap systems running along the trailing edge of the wing are common on all aircraft. The position of the leading-edge slats on an airliner (Airbus A310-300). In this picture, the slats are drooped.

  7. NACA airfoil - Wikipedia

    en.wikipedia.org/wiki/NACA_airfoil

    The NACA four-digit wing sections define the profile by: [2] First digit describing maximum camber as percentage of the chord. Second digit describing the distance of maximum camber from the airfoil leading edge in tenths of the chord. Last two digits describing maximum thickness of the airfoil as percent of the chord. [3]