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  2. Chord (aeronautics) - Wikipedia

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

    The wing, horizontal stabilizer, vertical stabilizer and propeller/rotor blades of an aircraft are all based on aerofoil sections, and the term chord or chord length is also used to describe their width. The chord of a wing, stabilizer and propeller is determined by measuring the distance between leading and trailing edges in the direction of ...

  3. Boeing 737 - Wikipedia

    en.wikipedia.org/wiki/Boeing_737

    The Boeing 737 MAX is the name given to the main models 737 MAX 7/8/9/10 series and the higher-density MAX 200 variant of the Boeing 737 family. It is offered in four main variants, typically offering 138 to 230 seats and a range of 3,215 to 3,825 nautical miles [nmi] (5,954 to 7,084 km; 3,700 to 4,402 mi).

  4. Thickness-to-chord ratio - Wikipedia

    en.wikipedia.org/wiki/Thickness-to-chord_ratio

    The natural outcome of this requirement is a wing design that is thin and wide, which has a low thickness-to-chord ratio. At lower speeds, undesirable parasitic drag is largely a function of the total surface area , which suggests using a wing with minimum chord, leading to the high aspect ratios seen on light aircraft and regional airliners .

  5. Leading-edge slat - Wikipedia

    en.wikipedia.org/wiki/Leading-edge_slat

    The chord of the slat is typically only a few percent of the wing chord. The slats may extend over the outer third of the wing, or they may cover the entire leading edge . Many early aerodynamicists, including Ludwig Prandtl , believed that slats work by inducing a high energy stream to the flow of the main airfoil , thus re-energizing its ...

  6. Aerodynamic center - Wikipedia

    en.wikipedia.org/wiki/Aerodynamic_center

    For symmetrical airfoils =, so the aerodynamic center is at 25% of chord measured from the leading edge. But for cambered airfoils the aerodynamic center can be slightly less than 25% of the chord from the leading edge, which depends on the slope of the moment coefficient, . These results obtained are calculated using the thin airfoil theory so ...

  7. Boeing 737 Next Generation - Wikipedia

    en.wikipedia.org/wiki/Boeing_737_Next_Generation

    Planform view of 737NG showing the 25% larger and 16-foot-wider (4.9 m) wing compared to the 737 Classic Boeing 737-800 glass cockpit The wing was redesigned with a new thinner airfoil section, and a greater chord and increased wing span (by 16 ft [4.9 m]) increased the wing area by 25%, which also increased total fuel capacity by 30%.

  8. 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.

  9. Aspect ratio (aeronautics) - Wikipedia

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

    If the wing is swept, c is measured parallel to the direction of forward flight. For most wings the length of the chord is not a constant but varies along the wing, so the aspect ratio AR is defined as the square of the wingspan b divided by the wing area S. [10] [11] In symbols, =.