Classical Aerodynamics of potential flow using Python and Jupyter Notebooks

Aircraft design optimization made fast through modern automatic differentiation. Written in Python, work in progress.

High-Power Rocketry 6 DOF Trajectory Simulation

Tucan is a free computer program for flight mechanics based on the unsteady vortex lattice method. Fully based in .NET.

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.

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

Mixed-fidelity unsteady aerodynamics and aeroacoustics

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

Vortex Lattice Method library written in Python

Easy aerodynamics in Python ✈️

☴🖩 Compressible Aerodynamics Calculator for Python

The minimum viable release of the Ptera Software Suite: a fast, easy-to-use, and opensource software package for analyzing flapping-wing flight.

CFD Code for Plasma and Reactive Flow

Vortex lattice method for inviscid lifting-surface aerodynamics

OpenFOAM case files for simulating NACA foils.

A Kerbal Space Program mod to display trajectory predictions, accounting for atmospheric drag, lift, etc.

Aircraft Conceptual Design Software

Fluid based shape optimization for the masses

CNN for airfoil lift-to-drag-ratio prediction

Calculate CdA (Coefficient of Drag) and crr (tire rolling resistance) based on field testing data in the form of Garmin or compatible .FIT files.

Computational Aerodynamics Lab

Blade Element Momentum Method for Propellers and Turbines

This project outputs G-code that is used to control a 4-axis hot wire cutter, employed to cut a wing / airfoil from a physical block of foam. Effectively, it is a slicer for a particular arrangement of raw-coordinate data files.

Simple, but realistic flight simulator controlled by mouse. You can modify aerodynamics of your plane easily by script-like files.

A code based on the Finite Volume Method discretisation of Navier-Stokes equations for simulation of compressible shear layer

Lift-Off Aerodynamics Software for Windows

多旋翼气动分析（设计）代码[Aerodynamic analysis codes for multi-rotors of helicopter/rotor-craft]

System identification for Monash UAS aircraft

makes ARMA 3's flights more realistic (GPWS, wind effect, etc.)