README.md

aero

Python packages for compressible flow computations

Features

• Mach dependent functions for isentropic total pressure, temperature and mass flow
• local Rankine-Hugoniot shock wave equations
• conical shock waves
• real gaz thermo functions
• kerozen thermo functions
• Fanno equations for momentum losses in a duct
• Rayleigh equations for heating/cooling in a duct
• misc: degree based trigo functions, Newton iterative solve, ODE integration

Installation & usage

• aero folder must be placed in a PYTHONPATH structure

• or append $PWDto your PYTHONPATH

  PYTHONPATH=$PWD:$PYTHONPATH python examples/test.py

Requirements

• numpy
• examples are plotted using matplotlib