Compressible Flow Calculator

This form calculates the properties of one-dimensional gas flow without losses (isentropic).
The required input is the Mach number of a point in the flow.
 
The gas can be changed by entering the value of Ratio of Specific Heats (γ).
 

Inputs Mach Number (M) Ratio of Specific Heats (γ)

Results   Dynamic Pressure/Static Pressure (q/p) Static Temperature/Total Temperature (T/TO) Static Pressure/Total Pressure (p/pO) Static Density/Total Density (ρ/rho;O) Local Area/Throat Area (A/A*)

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