Isentropic Compressible Flow Calculations   This form calculates the properties of one-dimensional air flow without losses (isentropic).The required input is the Mach number of a point in the flow. The gas is assumed to be ideal air.   Subsonic Tabulated Data   Supersonic Tabulated Data
Inputs Mach Number (M1)	Results   Dynamic Pressure/Static Pressure Ratio (q/p)   Static Temperature/Total Temperature Ratio (T/To)   Static Pressure/Total Pressure Ratio (P/Po)   Static Density/Total Density Ratio (rho/rhoo)   Local Area/Throat Area Ratio (A/A*)

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