Blade Element Momentum Theory Code for Positive and Negative Thrust Propellers

Blade-element-momentum theory code for predicting propeller performance at positive and negative thrust conditions for uniform inflow conditions. The code includes corrections for compressibility and root-tip effects and is able to handle the calculations for the operation of propellers in the energy-harvesting regime (negative thrust conditions).<br>For the validation data of the code, please refer to the paper "Benchmarking of Aerodynamic Models for Isolated Propellers Operating at Positive and Negative Thrust".<br>You will need to have suitable polar data of your propeller geometry to use this code. This code is written in MATLAB.<br>Check out the README.md file for instructions on how to use the code.