First Release using Direct Polar Storage

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.

Legacy Version

The "Legacy" branch of this repo is XROTOR as it was originally written. It uses a parametric model of the aerodynamic polars.

0.0.11

Added settings to control maximum number of iterations.

0.0.10

Improved polar fitting.

0.0.9

Switched back to returning boolean from XRotor.operate, and expose rm…

0.0.8

Return the rms from XRotor.operate instead of boolean to quantify con…

0.0.7

Bugfix

0.0.5

Fixed some import problems.