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Aerodynamics
Stagnation to Static Pressure in Compressible Flow Formulas
The Stagnation to Static Pressure ratio depends upon the Mach number and ratio of specific heats. And is denoted by P
r
.
Formulas to find Stagnation to Static Pressure in Compressible Flow
f
x
Ratio of Stagnation and Static Pressure
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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 Pressure?
The Stagnation to Static Pressure ratio depends upon the Mach number and ratio of specific heats.
Can the Stagnation to Static Pressure be negative?
{YesorNo}, the Stagnation to Static Pressure, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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