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  2. Normal shock tables - Wikipedia

    en.wikipedia.org/wiki/Normal_shock_tables

    In aerodynamics, the normal shock tables are a series of tabulated data listing the various properties before and after the occurrence of a normal shock wave. [1] With a given upstream Mach number , the post-shock Mach number can be calculated along with the pressure , density , temperature , and stagnation pressure ratios.

  3. Fanno flow - Wikipedia

    en.wikipedia.org/wiki/Fanno_flow

    The intersection points occur at the given initial Mach number and its post-normal shock value. For Figure 5, these values are M = 3 and 0.4752, which can be found the normal shock tables listed in most compressible flow textbooks. A given flow with a constant duct area can switch between the Fanno and Rayleigh models at these points.

  4. Thermodynamic relations across normal shocks - Wikipedia

    en.wikipedia.org/wiki/Thermodynamic_relations...

    "Normal shocks" are a fundamental type of shock wave. The waves, which are perpendicular to the flow, are called "normal" shocks. Normal shocks only happen when the flow is supersonic. At those speeds, no obstacle is identified before the speed of sound which makes the molecule return after sensing the obstacle.

  5. Mach number - Wikipedia

    en.wikipedia.org/wiki/Mach_number

    (In the case of a sharp object, there is no air between the nose and the shock wave: the shock wave starts from the nose.) As the Mach number increases, so does the strength of the shock wave and the Mach cone becomes increasingly narrow. As the fluid flow crosses the shock wave, its speed is reduced and temperature, pressure, and density increase.

  6. From garlic to grapes: Veterinarians shock pet owners with ...

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  7. Rankine–Hugoniot conditions - Wikipedia

    en.wikipedia.org/wiki/Rankine–Hugoniot_conditions

    A schematic diagram of a shock wave situation with the density , velocity , and temperature indicated for each region.. The Rankine–Hugoniot conditions, also referred to as Rankine–Hugoniot jump conditions or Rankine–Hugoniot relations, describe the relationship between the states on both sides of a shock wave or a combustion wave (deflagration or detonation) in a one-dimensional flow in ...

  8. Mach wave - Wikipedia

    en.wikipedia.org/wiki/Mach_wave

    A Mach wave is the weak limit of an oblique shock wave where time averages of flow quantities don't change (a normal shock is the other limit). If the size of the object moving at the speed of sound is near 0, then this domain of influence of the wave is called a Mach cone. [3] [4]

  9. A Comprehensive Guide to Navigating Your Dog’s Pregnancy - AOL

    www.aol.com/comprehensive-guide-navigating-dog...

    You can feed your female dog her normal diet for the first two stages. If you notice her lose weight during this period, add more food so she can maintain a healthy weight. Once she reaches about ...