compflow 0.5.0

Fast compressible flow tables for aerodynamic calculations in Python.

compflow

The compflow library contains functions to convert back and forth between Mach number and other non-dimensional groups in compressible flows. By using a NumPy--Fortran interface, the code is vectorised and lightning-fast, yielding a speed-up of up to two orders of magnitude.

Full documentation is available online.

Features

• Evaluation of ten non-dimensional flow quantities as explicit functions of Mach number;
• Iteration with Newton's method to invert explicit relations and solve for Mach number;
• Creation and caching of lookup tables to speed up inversions;
• Fortran-accelerated, fully-vectorised in both directions.

Basic usage

compflow is available on the Python Package Index, so installation is as simple as,

   python3 -m pip install compflow

Note: as the library uses Fortran subroutines behind the scenes, you will need a working Fortran compiler for the installation to complete successfully.

We can now start doing some calculations. First, an explicit evaluation of stagnation pressure ratio given a Mach number,

   >>> import compflow
   >>> ga = 1.4
   >>> compflow.Po_P_from_Ma(0.3, ga)
   1.0644302861529382

Second, an inversion of flow function where iterative solution for Mach number is required,

   >>> compflow.Ma_from_mcpTo_APo(0.8, ga)
   0.39659360325173604

The names and symbols of non-dimensional quantities are fairly self-explanatory, but a full list is given in the Nomenclature. All functions and the equations used for the calculations are documented in the API.

Numpy arrays are also accepted as inputs,

   >>> import numpy
   >>> Ma1 = numpy.array([0., 0.5, 1., 2.])
   >>> compflow.To_T_from_Ma(Ma1, ga)
   array([1.  , 1.05, 1.2 , 1.8 ])
   >>> Ma2 = numpy.array([[0.1, 0.2], [0.3, 0.4], [0.5, 0.6]])
   >>> compflow.To_T_from_Ma(Ma2, ga)
   array([[1.002, 1.008],
          [1.018, 1.032],
          [1.05 , 1.072]])

When solving for Mach number at a given normalised mass flow, it is assumed that we are on the subsonic branch of the curve unless a flag is specified. Where no solution is possible, i.e. if the flow would choke, NaN is returned,

   >>> capacity = [0.6, 2.]
   >>> compflow.Ma_from_mcpTo_APo(capacity, ga)
   array([0.28442265,        nan])
   >>> compflow.Ma_from_mcpTo_APo(capacity, ga, sup=True)
   array([2.27028708,        nan])

TODO

• Sort out packaging so that NumPy gets installed automatically (distutils due to be deprecated?).

James Brind Mar 2022