aerokit 1.2.1
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Description:
aerokit 1.2.1
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) 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
Installation & usage
pip install aerokit
Documentation is available on readthedocs. More examples are available in the repository.
Requirements
numpy, scipy
examples are plotted using matplotlib
License:
For personal and professional use. You cannot resell or redistribute these repositories in their original state.
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