Rankine-Hugoniot Shock Pressure Relation Calculator
Ratio of Specific Heats
Mach Number
Pressure Ratio: {{pressureRatioResult() | number:4}}

Formula:

p2 / p1 = (2γM12 - (γ-1) ) / (γ+1)

Where,

p2 / p1 = Rankine-Hugoniot Relation of Pressure

p1 = Initial Pressure

p2 = Final Pressure

γ = Ratio of Specific Heats

M1 = Mach Number