Temperature Ratio in Hypersonic Flow Formulas

The Temperature Ratio is the comparison of temperatures before and after an oblique shock wave, indicating how energy is transformed in hypersonic flow conditions. And is denoted by T_ratio.

Formulas to find Temperature Ratio in Hypersonic Flow

fxTemperature Ratio when Mach Becomes InfiniteGo

fxTemperature RatiosGo

List of variables in Hypersonic Flow formulas

fx Specific Heat Ratio Go

fx Mach Number Go

fx Wave Angle Go

fx Pressure Ratio Go

fx Density Ratio Go

FAQ

What is the Temperature Ratio?

The Temperature Ratio is the comparison of temperatures before and after an oblique shock wave, indicating how energy is transformed in hypersonic flow conditions.

Can the Temperature Ratio be negative?

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

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