aerokit
Python packages for compressible flow computations
Features
- Mach dependent functions for isentropic total pressure, temperature and mass flow
- local Rankine-Hugoniot shock wave equations (or 2d planar shocks)
- conical shock waves
- Fanno equations for momentum losses in a duct
- Rayleigh equations for heating/cooling in a duct
- unsteady compressible 1D flows
- applications: nozzle flows and (Riemann) shock tube
- misc: degree based trigo functions
Installation & usage
pip install aerokit
Documentation is available on readthedocs. More examples are available in the repository.
Requirements
numpyscipy- examples are plotted using
matplotlib