Mach Number behind shock in Hypersonic Inviscid Flow Formulas

Mach Number behind shock is the Mach number over the body after a shockwave has occurred. And is denoted by M₂.

Formulas to find Mach Number behind shock in Hypersonic Inviscid Flow

fxMach Wave behind ShockGo

fx Freestream Velocity Go

fx Local Shock Velocity for Mach Wave Go

fx Speed of Sound Go

What is the Mach Number behind shock?

Mach Number behind shock is the Mach number over the body after a shockwave has occurred.

Can the Mach Number behind shock be negative?

{YesorNo}, the Mach Number behind shock, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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