aerodynamics

Source-Doublet Panel Method

Discrete Adjoint for Rapid Transonic Flows

Processing scripts for the MechaRaptor experimental data.

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

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

Field panel method for quickly solving 3D transonic flows

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

Database for rotor geometries and associated experimental data.

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

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

Experimental analysis of a large-scale tandem flapping wings system.

This presentation is scheduled to be given at SciTech 2023 in National Harbor, MD, USA.