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  2. Speed of sound - Wikipedia

    en.wikipedia.org/wiki/Speed_of_sound

    A graph comparing results of the two equations is to the right, using the slightly more accurate value of 331.5 m/s (1,088 ft/s) for the speed of sound at 0 °C. [ 11 ] : 120 -121 Effects due to wind shear

  3. Mach number - Wikipedia

    en.wikipedia.org/wiki/Mach_number

    c is the speed of sound in the medium, which in air varies with the square root of the thermodynamic temperature. By definition, at Mach 1, the local flow velocity u is equal to the speed of sound. At Mach 0.65, u is 65% of the speed of sound (subsonic), and, at Mach 1.35, u is 35% faster than the speed of sound (supersonic).

  4. U.S. Standard Atmosphere - Wikipedia

    en.wikipedia.org/wiki/U.S._Standard_Atmosphere

    Comparison of the 1962 US Standard Atmosphere graph of geometric altitude against air density, pressure, the speed of sound and temperature with approximate altitudes of various objects. [ 1 ] The U.S. Standard Atmosphere is a static atmospheric model of how the pressure , temperature , density , and viscosity of the Earth's atmosphere change ...

  5. Sound speed profile - Wikipedia

    en.wikipedia.org/wiki/Sound_speed_profile

    Figure 1. Table 1's data in graphical format. Although given as a function of depth [note 1], the speed of sound in the ocean does not depend solely on depth.Rather, for a given depth, the speed of sound depends on the temperature at that depth, the depth itself, and the salinity at that depth, in that order.

  6. Talk:Speed of sound - Wikipedia

    en.wikipedia.org/wiki/Talk:Speed_of_sound

    39 Sound speed in seawater - MacKenzie vs. graph. ... 70's sound speed equations were all the rage.) ... determine the speed of sound at the altitude where the sound ...

  7. Equivalent airspeed - Wikipedia

    en.wikipedia.org/wiki/Equivalent_airspeed

    where a 0 is 1,225 km/h (661.45 kn) (the standard speed of sound at 15 °C), M is the Mach number, P is static pressure, and P 0 is standard sea level pressure (1013.25 hPa). Combining the above with the expression for Mach number gives EAS as a function of impact pressure and static pressure (valid for subsonic flow):

  8. Chapman–Jouguet condition - Wikipedia

    en.wikipedia.org/wiki/Chapman–Jouguet_condition

    The energy release re-accelerates the flow back to the local speed of sound. It can be shown fairly simply, from the one-dimensional gas equations for steady flow, that the reaction must cease at the sonic ("CJ") plane, or there would be discontinuously large pressure gradients at that point.

  9. Acoustic theory - Wikipedia

    en.wikipedia.org/wiki/Acoustic_theory

    The boundary conditions required to solve for the potential come from the fact that the velocity of the fluid must be 0 normal to the fixed surfaces of the system. Taking the time derivative of this wave equation and multiplying all sides by the unperturbed density, and then using the fact that p ′ = ρ 0 ∂ ϕ ∂ t {\displaystyle p'=\rho ...