Temperature Ratio across Shock in Hypersonic Inviscid Flow Formulas

Temperature ratio across shock is the ratio of downstream temperature to upstream temperature across the shock wave. And is denoted by Tshock_ratio.

Formulas to find Temperature Ratio across Shock in Hypersonic Inviscid Flow

fxRatio of New and Old Temperature for Expansion WavesGo

fxRatio of New and Old TemperatureGo

fx Specific Heat Ratio Go

fx Normal velocity Go

fx Old Speed of Sound Go

What is the Temperature Ratio across Shock?

Temperature ratio across shock is the ratio of downstream temperature to upstream temperature across the shock wave.

Can the Temperature Ratio across Shock be negative?

{YesorNo}, the Temperature Ratio across Shock, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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