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  2. Supercritical airfoil - Wikipedia

    en.wikipedia.org/wiki/Supercritical_airfoil

    Supercritical airfoils feature four main benefits: they have a higher drag-divergence Mach number, [21] they develop shock waves farther aft than traditional airfoils, [22] they greatly reduce shock-induced boundary layer separation, and their geometry allows more efficient wing design (e.g., a thicker wing and/or reduced wing sweep, each of which may allow a lighter wing).

  3. Minecraft modding - Wikipedia

    en.wikipedia.org/wiki/Minecraft_modding

    The popularity of Minecraft mods has been credited for helping Minecraft become one of the best-selling video games of all time. The first Minecraft mods worked by decompiling and modifying the Java source code of the game. The original version of the game, now called Minecraft: Java Edition, is still modded this way, but with more advanced tools.

  4. Drag-divergence Mach number - Wikipedia

    en.wikipedia.org/wiki/Drag-divergence_Mach_number

    Two of the important technological advancements that arose out of attempts to conquer the sound barrier were the Whitcomb area rule and the supercritical airfoil. A supercritical airfoil is shaped specifically to make the drag-divergence Mach number as high as possible, allowing aircraft to fly with relatively lower drag at high subsonic and ...

  5. Talk:Supercritical airfoil/Archive 1 - Wikipedia

    en.wikipedia.org/wiki/Talk:Supercritical_airfoil/...

    3 Supercritical airfoil Mach Number/pressure coefficient diagram. ... 6 This article is about what is good about these wings. 1 comment. Toggle the table of contents.

  6. Vortilon - Wikipedia

    en.wikipedia.org/wiki/Vortilon

    Experimental Vought F-8 Crusader with supercritical wing. The supercritical wing would have been prone to pitch-up as the wing had increased sweep and aspect ratio compared to the standard wing. No pitch-up problems were experienced with vortilons fitted. [14] [15] Bombardier Challenger 300, later becoming the Challenger 350 & new 3500 series.

  7. Wave drag - Wikipedia

    en.wikipedia.org/wiki/Wave_drag

    The supercritical airfoil is a type that results in reasonable low speed lift like a normal airfoil, but has a profile considerably closer to that of the von Kármán ogive. All modern civil airliners use forms of supercritical aerofoil and have substantial supersonic flow over the wing upper surface.

  8. Shock stall - Wikipedia

    en.wikipedia.org/wiki/Shock_stall

    A shock stall is a stall created when the airflow over an aircraft's wings is disturbed by shock waves formed when flying at or above the aircraft's drag divergence Mach number. Shock stall may cause control problem during speed transition (transonic to supersonic). Thin supercritical wing section and swept-back wing can postpone shock stall to ...

  9. NACA airfoil - Wikipedia

    en.wikipedia.org/wiki/NACA_airfoil

    The NACA four-digit wing sections define the profile by: [2] First digit describing maximum camber as percentage of the chord. Second digit describing the distance of maximum camber from the airfoil leading edge in tenths of the chord. Last two digits describing maximum thickness of the airfoil as percent of the chord. [3]

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