Functions for working with compressible inviscid flow of gases.
This package provide a class for the most common function used in calculations of supersonic flow of an ideal gas, including adiabatic flow properties, normal shock wave properties, theta-beta-Mach relation, and Prandtl-Meyer function.
pip install -i compressible-flow
Create an Ideal_Gas using the adiabatic ratio $\gamma$ and the effective gas constant $R_{specific}=R/M$ as parameters
import compressible_flow as cf
air = cf.Ideal_Gas(R=287, gamma=1.4)
Calculate the total temperature to temperature ratio T_0/T as a function of the Mach number
air.T0T(M=1.5)
https://gitlab.com/itorre/compressible_flow
This project is released under the MIT license.
FAQs
Functions for working with compressible inviscid flow of gases
We found that compressible-flow demonstrated a healthy version release cadence and project activity because the last version was released less than a year ago. It has 1 open source maintainer collaborating on the project.
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