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  2. Droop nose (aeronautics) - Wikipedia

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

    The first supersonic delta to receive a drooped nose was the Fairey Delta 2, a British experimental high-speed aircraft. Nicknamed "Droop Snoot", [ 1 ] the Delta 2 featured a relatively long tapered nose, which smoothly flowed into its cylindrical cross-section fuselage , to generate a high level of aerodynamic efficiency. [ 2 ]

  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. 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, the delta wing did not find significant practical applications until the Jet Age , when it proved suitable for high-speed subsonic and supersonic flight. [ 1 ]

  5. Dyke Delta - Wikipedia

    en.wikipedia.org/wiki/Dyke_Delta

    JD-1 Dyke Delta - a small version, with 1+2 seating and fixed landing gear, used to generate and verify delta-wing and tailless-configuration flight characteristics. First flight July 1962; destroyed June 1964. [4] JD-2 Dyke Delta - an updated and enlarged version, with 1+3 seating and retractable landing gear. Debuted at Experimental Aircraft ...

  6. Strake (aeronautics) - Wikipedia

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

    Nose, wing and ventral strakes Vortices over the wing strakes of an F/A-18E Super Hornet. In aviation, a strake is an aerodynamic surface generally mounted on the fuselage of an aircraft to improve the flight characteristics either by controlling the airflow (acting as large vortex generators) or by a simple stabilising effect.

  7. 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 ...

  8. Area rule - Wikipedia

    en.wikipedia.org/wiki/Area_rule

    For example, consider that at Mach 1.3 the angle of the Mach cone generated by the nose of the aircraft will be at an angle μ = arcsin(1/M) = 50.3° (where μ is the angle of the Mach cone, also known as Mach angle, and M is the Mach number). In this case the "perfect shape" is biased rearward; therefore, aircraft designed for lower wave drag ...

  9. Convair XF-92 - Wikipedia

    en.wikipedia.org/wiki/Convair_XF-92

    The Convair XF-92 (re-designated from XP-92 in 1948) is an American, delta wing, first-generation jet prototype. Originally conceived as a point-defence interceptor, the design was later used purely for experimental purposes and only one was built.