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 of Blunt-Nosed Cylinder (First Approximation)Go

fxPressure Ratio for Unsteady Waves with Subtracted Induced Mass Motion for Expansion WavesGo

fxPressure Ratio for Unsteady WavesGo

fxPressure Ratio for Cold-Wall Case Strong InteractionGo

fxPressure Ratio for Cold-Wall Case Weak InteractionGo

fx Mach Number Cylinder Go

fx Drag Coefficient Go

fx Distance from X-Axis Go

fx Diameter Go

fx Specific Heat Ratio Go

fx Induced Mass Motion Go

fx Speed of Sound Go

fx Viscous Interaction 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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