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Aerodynamics
Mach Number Behind Normal Shock in Normal Shock Wave Formulas
Mach Number Behind Normal Shock represents the velocity of a fluid or airflow relative to the speed of sound after passing through a normal shock wave. And is denoted by M
2
.
Formulas to find Mach Number Behind Normal Shock in Normal Shock Wave
f
x
Mach Number behind Shock
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List of variables in Normal Shock Wave formulas
f
x
Specific Heat Ratio
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f
x
Mach Number Ahead of Normal Shock
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FAQ
What is the Mach Number Behind Normal Shock?
Mach Number Behind Normal Shock represents the velocity of a fluid or airflow relative to the speed of sound after passing through a normal shock wave.
Can the Mach Number Behind Normal Shock be negative?
{YesorNo}, the Mach Number Behind Normal Shock, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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