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  2. 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.

  3. 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 ...

  4. Flying wing - Wikipedia

    en.wikipedia.org/wiki/Flying_wing

    The concept of the flying wing was born on 16 February 1876 when French engineers Alphonse Pénaud and Paul Gauchot filed a patent for an aero-plane or flying aircraft [5] powered by two propellers and with all the characteristics of a flying wing as we know it today. [6] Tailless aircraft have been experimented with since the earliest attempts ...

  5. Leading edge - Wikipedia

    en.wikipedia.org/wiki/Leading_edge

    Seen in plan the leading edge may be straight or curved. A straight leading edge may be swept or unswept, the latter meaning that it is perpendicular to the longitudinal axis of the aircraft. As wing sweep is conventionally measured at the 25% chord line [3] an unswept wing may have a swept or

  6. Swept wing - Wikipedia

    en.wikipedia.org/wiki/Swept_wing

    A straight-winged North American FJ-1 flying next to a swept-wing FJ-2 in 1952.. There are three main reasons for sweeping a wing: [1] 1. to arrange the center of gravity of the aircraft and the aerodynamic center of the wing to coincide more closely for longitudinal balance, e.g. Messerschmitt Me 163 Komet and Messerschmitt Me 262.

  7. Wing loading - Wikipedia

    en.wikipedia.org/wiki/Wing_loading

    Wing loading is a useful measure of the stalling speed of an aircraft. Wings generate lift owing to the motion of air around the wing. Larger wings move more air, so an aircraft with a large wing area relative to its mass (i.e., low wing loading) will have a lower stalling speed.

  8. This radical plane concept with an all-in-one wing could be ...

    www.aol.com/radical-plane-concept-one-wing...

    "Blended wing" aircraft could be the future of commercial aviation. ... While a blended-wing passenger plane is a relatively new concept, the aircraft type has been flying for the US military for ...

  9. Angle of attack - Wikipedia

    en.wikipedia.org/wiki/Angle_of_attack

    As the angle of attack of a fixed-wing aircraft increases, separation of the airflow from the upper surface of the wing becomes more pronounced, leading to a reduction in the rate of increase of the lift coefficient. The figure shows a typical curve for a cambered straight wing. Cambered airfoils are curved such that they generate some lift at ...