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*)
 

(c) 2006 AMME, University of Sydney.