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  2. Supercritical airfoil - Wikipedia

    en.wikipedia.org/wiki/Supercritical_airfoil

    A supercritical aerofoil (supercritical airfoil in American English) is an airfoil designed primarily to delay the onset of wave drag in the transonic speed range. Supercritical airfoils are characterized by their flattened upper surface, highly cambered ("downward-curved") aft section, and larger leading-edge radius compared with NACA 6-series ...

  3. Richard T. Whitcomb - Wikipedia

    en.wikipedia.org/wiki/Richard_T._Whitcomb

    After World War II, NACA research began to focus on near-sonic and low-supersonic airflow.After considering the sudden drag increase which a wing-fuselage combination experiences at somewhere around 500 mph (800 km/h), Whitcomb concluded that "the disturbances and shock waves are simply a function of the longitudinal variation of the cross-sectional area" – that is, the effect of the wings ...

  4. Anti-shock body - Wikipedia

    en.wikipedia.org/wiki/Anti-shock_body

    Anti-shock body is the name given by Richard T. Whitcomb to a pod positioned on the upper surface of a wing. [1] Its purpose is to reduce wave drag while travelling at transonic speeds (Mach 0.8–1.0), which includes the typical cruising range of conventional jet airliners.

  5. Area rule - Wikipedia

    en.wikipedia.org/wiki/Area_rule

    Designers at Armstrong-Whitworth took the sonic area rule a step further in their proposed M-Wing, in which the wing was first swept forward and then to the rear. This allowed the fuselage to be narrowed in front of the root as well as behind it, leading to a smoother fuselage that remained wider on average than one using a classic swept wing.

  6. Shock stall - Wikipedia

    en.wikipedia.org/wiki/Shock_stall

    Thin supercritical wing section and swept-back wing can postpone shock stall to higher speed. [1] A stall is the decrease in lift to a value below the weight, and the associated increase in drag upon the separation of the boundary layer (in this case behind the shock wave).

  7. Supersonic airfoils - Wikipedia

    en.wikipedia.org/wiki/Supersonic_airfoils

    Years of research and experience with the unusual conditions of supersonic flow have led to some interesting conclusions about airfoil design. Considering a rectangular wing, the pressure at a point P with coordinates (x,y) on the wing is defined only by the pressure disturbances originated at points within the upstream Mach cone emanating from point P. [3] As result, the wing tips modify the ...

  8. William Shatner explains why his classic 'Twilight Zone ... - AOL

    www.aol.com/entertainment/william-shatner...

    Donner, of course, would later go on to direct blockbusters like Superman: The Movie and The Omen, but Shatner says that the young director didn't exactly have the time on the "Nightmare" set to ...

  9. Supercritical - Wikipedia

    en.wikipedia.org/wiki/Supercritical

    Supercritical fluid, a substance at a temperature and pressure above its thermodynamic critical point: Supercritical carbon dioxide: Supercritical fluid chromatography, a form of liquid chromatography using supercritical carbon dioxide as the mobile phase; Supercritical water:

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