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  2. Delta wing - Wikipedia

    en.wikipedia.org/wiki/Delta_wing

    A delta wing is a wing shaped in the form of a triangle. It is named for its similarity in shape to the Greek uppercase letter delta (Δ). Although long studied, it did not find significant applications until the Jet Age , when it proved suitable for high-speed subsonic and supersonic flight.

  3. List of delta-wing aircraft - Wikipedia

    en.wikipedia.org/wiki/List_of_delta-wing_aircraft

    Ogival delta wing fitted to a Fairey Delta 2 to test the Concorde design. Boeing X-32: US: Supersonic: Fighter: 2000: Prototype: Tailless JSF contender. Boulton Paul ...

  4. Dassault MD.750 - Wikipedia

    en.wikipedia.org/wiki/Dassault_MD.750

    The delta wing is mounted low and extends most of the length of the fuselage aft of the intakes, as with other Mirage fighters, and it has a single vertical tail but uses square section intake ramps with a linear shock plate rather than shock cones, as used on the North American A-5 Vigilante and Mikoyan-Gurevich MiG-25 unlike other Mirage ...

  5. Canard (aeronautics) - Wikipedia

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

    In the close-coupled delta wing canard, the foreplane is located just above and forward of the wing. The vortices generated by a delta-shaped foreplane flow back past the main wing and interact with its own vortices. Because these are critical for lift, a badly-placed foreplane can cause severe problems.

  6. Boulton Paul P.111 - Wikipedia

    en.wikipedia.org/wiki/Boulton_Paul_P.111

    The delta wing of the P.111 was relatively thin in comparison to contemporary wings and was swept at an angle of 45°. [4] When not fitted with tip extensions, this wing was strongly cropped at about 75 percent of the pure delta shape, while the installation of the larger extensions resulted in an almost unbroken pure delta shape.

  7. Tailless aircraft - Wikipedia

    en.wikipedia.org/wiki/Tailless_aircraft

    The long wing span also reduces manoeuvrability, and for this reason Dunne's design was rejected by the British Army. An alternative is the use of low or null pitching moment airfoils, seen for example in the Horten series of sailplanes and fighters. These use an unusual wing aerofoil section with reflex or reverse camber on the rear or all of ...

  8. General Dynamics F-16XL - Wikipedia

    en.wikipedia.org/wiki/General_Dynamics_F-16XL

    The wing and rear horizontal control surfaces of the base F-16A were replaced with a cranked-arrow delta wing 115% larger than the original wing. [15] Extensive use of graphite-bismaleimide composites allowed the savings of 595 pounds (270 kg) of weight, [ 16 ] but the F-16XL-1 and XL-2 were 4,100 pounds (1,900 kg) and 5,600 pounds (2,500 kg ...

  9. ‘Everybody screamed’: 35 years after Delta 1141 ... - AOL

    www.aol.com/everybody-screamed-35-years-delta...

    After 22 seconds of terror, the Delta jet smashed through antennas about 1,000 feet beyond the runway 18L and slid sideways into a field on the south end of the airport, disintegrating the right wing.