There are 12 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.
NeuralFoil is an airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
CEASIOMpy is a Python conceptual aircraft design environment
A freeware hobby project simulation for X-Plane of the Boeing 777-300ER
A Comprehensive Julia implementation of the Vortex Lattice Method
xflrpy is a python enabled version of xflr5 for scripting and design optimization.
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 Julia package to import geometry created using OpenVSP into Julia
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.
: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.
This project introduces a fault detection framework using neural networks for the RCAM. The study begins by remodeling the RCAM’s nonlinear dynamics to simulate various fault conditions. Subsequently, data generated from these faulty models underpin the training and testing of neural networks.
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!