aerodynamics

Discrete Adjoint for Rapid Transonic Flows

Source-Doublet Panel Method

Processing scripts for the MechaRaptor experimental data.

A Free Open-Source Blade Element Momentum Theory implementation in Matlab.

Toolbox for analysis of airfoils and related data (polars, geometries, etc) with Matlab.

MechaRaptor Data for the first test campaign in Q4 2022 (Rectangular flat plates 4mm)

Analysis and optimization cases for DART

Safety report, operating manuals and generic documentation for the MechaRaptor setup.

Database for rotor geometries and associated experimental data.

Complete documentation for Rotare, a feature-rich and open-source implementation of the BEMT in Matlab.

Field panel method for quickly solving 3D transonic flows