AeroKit

Python packages for compressible flow computations

Mach dependent functions for isentropic total pressure, temperature and mass flow
local Rankine-Hugoniot shock wave equations (or 2d planar shocks) and conical shock waves
Fanno equations for momentum losses in a duct
Rayleigh equations for heating/cooling in a duct
unsteady compressible 1D flows
1D stability equations: Orr-Sommerfeld and linearized compressible inviscid
applications:
nozzle flows
(Riemann) shock tube
Channel incompressible flow stability (Poiseuille)
degree based trigonometric functions
real gaz and kerozen thermo functions
Newton iterative solve, ODE integration, Chebyshev spectral discretization

pip install aerokit

Documentation is available on readthedocs. More examples are available in the repository.