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Aerodynamics
Stagnation to Static Temperature in Compressible Flow Formulas
The Stagnation to Static Temperature ratio depends upon the Mach number and ratio of specific heats. And is denoted by T
r
.
Formulas to find Stagnation to Static Temperature in Compressible Flow
f
x
Ratio of Stagnation and Static Temperature
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List of variables in Compressible Flow formulas
f
x
Specific Heat Ratio
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f
x
Mach Number
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FAQ
What is the Stagnation to Static Temperature?
The Stagnation to Static Temperature ratio depends upon the Mach number and ratio of specific heats.
Can the Stagnation to Static Temperature be negative?
{YesorNo}, the Stagnation to Static Temperature, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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