| 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
