There are 11 repositories under aircraft-design topic.
An open source flight dynamics & control software library
Aircraft design optimization made fast through modern automatic differentiation. Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.
Ptera Software is a fast, easy-to-use, and open-source software package for analyzing flapping-wing flight.
CEASIOMpy is a Python conceptual aircraft design environment
NeuralFoil is an airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
A freeware hobby project simulation for X-Plane of the Boeing 777-300ER
xflrpy is a python enabled version of xflr5 for scripting and design optimization.
A Comprehensive Julia implementation of the Vortex Lattice Method
Aircraft Conceptual Design Software
In this repository I publish the python code, that was part of my master thesis. The thesis can be found here, however its in German though, sry. :/
Get airfoil characteristics from an experimental database.
A Python implementation of the 1976 standard atmosphere model. Suitable to determine air properties at different altitudes.
The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and frequency domain as well as dynamic landing loads based on a generic landing gear module.
PteraControls is a tool for designing control systems for flapping wing vehicles.
:chart_with_upwards_trend: Program that calculates design parameters for an ornithopter in level flight
The study aims to develop a preliminary design of a fixed-wing aerodyne (Business Jet) able to carry a reduced number of people in intercontinental flights at the maximum possible Mach number.
A Python script written to perform aircraft weight estimations and inertia calculations
Read and write CPACS files. Create an object structure out of CPACS and develop faster.
A Julia package to import geometry created using OpenVSP into Julia
:chart_with_upwards_trend: Simulation of an oscillating airfoil
Part 21 DOA Design Software written in Tkinter
UCSD SE262: Aircraft Structural Repair. Programs used to solve aircraft structural problems.
Simulation model predicting the performance of a propeller using the Blade Element Theory.
My Zettelkasten univerisity notes on computational fluid dynamics, aircraft propulsion systems, and aerodynamics.
A great tool to ease the Calculations for Aircraft Design Project. Everything's Automated, give the required values and ADPHelper will do everything for you!
Wing optimization
Paper Air Challenge plane design