Going forward, XROTOR will handle the aerodynamic polars of blade sections differently. Starting with this version, polars are stored directly as a table of angles of attack, lift coefficients, drag coefficients, and moment coefficients instead of a parameterized model of the polars.
0.1.0
The "Legacy" branch of this repo is XROTOR as it was originally written. It uses a parametric model of the aerodynamic polars.