compressible-flow 0.1.4

Functions for working with compressible inviscid flow of gases

Compressible_flow

Functions for working with compressible inviscid flow of gases.

Description

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.

Installation

pip install -i compressible-flow

Usage

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)

Repository

https://gitlab.com/itorre/compressible_flow

License

This project is released under the MIT license.