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AeroKit

Python packages for compressible flow computations

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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

Metadata

Release files for aerokit 1.5.0

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aerokit-1.5.0-py3-none-any.whl Python 3 none any Details for aerokit-1.5.0-py3-none-any.whl

Total release size: 124.5 kB

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