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 Ratio (q/p)