Mach Number Ahead of Normal Shock in Normal Shock Wave Formulas

Mach Number Ahead of Normal Shock represents the velocity of a fluid or airflow relative to the speed of sound before encountering a normal shock wave. And is denoted by M₁.

Normal Shock Wave formulas that make use of Mach Number Ahead of Normal Shock

fxMach Number behind ShockGo

fxStagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formulaGo

fxStatic Pressure behind Normal Shock for given Upstream Pressure and Mach NumberGo

fxStatic Temperature behind Normal Shock for given Upstream Temperature and Mach NumberGo

fxStatic Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach NumberGo

fxShock StrengthGo

fxDensity Ratio across Normal ShockGo

fxPressure Ratio across Normal ShockGo

fxTemperature Ratio across Normal ShockGo

fxStatic Enthalpy Ratio across Normal ShockGo

FAQ

What is the Mach Number Ahead of Normal Shock?

Mach Number Ahead of Normal Shock represents the velocity of a fluid or airflow relative to the speed of sound before encountering a normal shock wave.

Can the Mach Number Ahead of Normal Shock be negative?

{YesorNo}, the Mach Number Ahead of Normal Shock, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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