Pressure Ratio in Hypersonic Flow Formulas

Pressure Ratio is ratio of final to initial pressure. And is denoted by r_p.

Formulas to find Pressure Ratio in Hypersonic Flow

fxPressure Ratio for High Mach NumberGo

fxPressure Ratio having High Mach Number with Similarity ConstantGo

fx Mach Number ahead of Shock Go

fx Mach Number Behind Shock Go

fx Specific Heat Ratio Go

fx Hypersonic Similarity Parameter Go

What is the Pressure Ratio?

Pressure Ratio is ratio of final to initial pressure.

Can the Pressure Ratio be negative?

{YesorNo}, the Pressure Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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