Classical Aerodynamics of potential flow using Python and Jupyter Notebooks

Aircraft design optimization made fast through computational graph transformations (e.g., automatic differentiation). Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.

Next generation High-Power Rocketry 6-DOF Trajectory Simulation

A parametric aircraft geometry tool

An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy

DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization

OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.

Ptera Software is a fast, easy-to-use, and open-source software package for analyzing flapping-wing flight.

A list of aerospace engineering learning resources 🚀✈️

A Large-Scale Multimodal Car Dataset with Computational Fluid Dynamics Simulations and Deep Learning Benchmarks

NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.

Model Rocket Simulator oriented to the design and tuning of active control systems, be them in the form of TVC, Active Fin Control or just parachute deployment algorithms on passively stable rockets. It is able to simulate non-linear actuator dynamics and has some limited Software in the Loop capabilities. The program computes all the subsonic a…

Matlab implementation to simulate the non-linear dynamics of a fixed-wing unmanned areal glider. Includes tools to calculate aerodynamic coefficients using a vortex lattice method implementation, and to extract longitudinal and lateral linear systems around the trimmed gliding state.

Fast and accurate aerodynamic modeling using general numerical lifting-line theory.

Library for Aircraft Dynamics And Control

CEASIOMpy is a Python conceptual aircraft design environment

Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique in many ways, while the most prominent feature is that it is entirely based in .NET. Recompiling the project is very easy and you can have tons of fun extending the source code.

Blade Element Momentum Method for Propellers and Turbines

6-DOF Rocket Flight Simulation Framework