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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. Category:Delta-wing aircraft - Wikipedia

    en.wikipedia.org/wiki/Category:Delta-wing_aircraft

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  5. Lockheed Martin X-44 MANTA - Wikipedia

    en.wikipedia.org/wiki/Lockheed_Martin_X-44_MANTA

    It was intended to test the feasibility of full yaw, pitch and roll authority without tailplanes (horizontal or vertical). Attitude control would rely purely on 3D thrust vectoring. [1] The aircraft design was derived from the F-22 Raptor and featured a stretched delta wing without tail surfaces. [1]

  6. List of tailless aircraft - Wikipedia

    en.wikipedia.org/wiki/List_of_tailless_aircraft

    Tailess VTOL delta wing. Hispano HA P-300 (HA-23P) Spain: Glider: Experimental: 1959/60: Prototype: 1: Developed into the Egyptian Helwan HA-300 tailed jet. Hoffman ...

  7. Dassault Rafale - Wikipedia

    en.wikipedia.org/wiki/Dassault_Rafale

    The Rafale was developed as a modern jet fighter with a very high level of agility; Dassault chose to combine a delta wing with active close-coupled canard to maximize manoeuvrability. The aircraft is capable of withstanding from −3.6 g to 9 g (10.5 g on Rafale solo display and a maximum of 11 g can be reached in case of emergency [ 69 ] [ 70

  8. Boulton Paul P.111 - Wikipedia

    en.wikipedia.org/wiki/Boulton_Paul_P.111

    The resulting aircraft, designated P.111, was a basic aircraft specifically designed for Delta wing research. [1] In terms of its basic configuration, the P.111 was designed to be the smallest possible airframe that would accommodate both a single Rolls-Royce Nene turbojet engine, a Martin-Baker-built ejection seat and a delta wing.

  9. Chengdu J-10 - Wikipedia

    en.wikipedia.org/wiki/Chengdu_J-10

    Shenyang's proposal was based on its cancelled J-13 with a F-16-like strake-wing. Hongdu's proposal was MiG-23/Su-24-like with variable-sweep wing. Chengdu Aircraft Design Institute's (CADI) proposal was a Saab 37 Viggen-like design based on its cancelled J-9. [8] CADI's proposal was selected in February 1984.