aerodynamics
There are 247 repositories under aerodynamics topic.
barbagroup/AeroPython
Classical Aerodynamics of potential flow using Python and Jupyter Notebooks
peterdsharpe/AeroSandbox
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.
RocketPy-Team/RocketPy
Next generation High-Power Rocketry 6-DOF Trajectory Simulation
OpenVSP/OpenVSP
A parametric aircraft geometry tool
byuflowlab/FLOWUnsteady
An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy
Mohamedelrefaie/DrivAerNet
A Large-Scale Multimodal Car Dataset with Computational Fluid Dynamics Simulations and Deep Learning Benchmarks
mdolab/dafoam
DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization
mdolab/OpenAeroStruct
OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
camUrban/PteraSoftware
Ptera Software is a fast, easy-to-use, and open-source software package for analyzing flapping-wing flight.
mahran-sayed/awesome-aerospace-engineering
A list of aerospace engineering learning resources 🚀✈️
peterdsharpe/NeuralFoil
NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
GuidodiPasquo/AeroVECTOR
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 aerodynamic parameters of interest and integrates the 3DOF Equations of Motion to simulate the complete flight.
jrgenerative/fixed-wing-sim
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.
usuaero/MachUpX
Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
iff-gsc/LADAC
Library for Aircraft Dynamics And Control
cfsengineering/CEASIOMpy
CEASIOMpy is a Python conceptual aircraft design environment
OpenVOGEL/Tucan
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.
byuflowlab/CCBlade.jl
Blade Element Momentum Method for Propellers and Turbines
henrystoldt/MAPLEAF
6-DOF Rocket Flight Simulation Framework
nikhil-sethi/xflrpy
xflrpy is a python enabled version of xflr5 for scripting and design optimization.
bernardparent/CFDWARP
Computational Fluid Dynamics, Waves, Reactions, Plasmas
petebachant/NACAFoil-OpenFOAM
OpenFOAM case files for simulating NACA foils.
byuflowlab/FLOWVLM
Vortex lattice method for inviscid lifting-surface aerodynamics
aqreed/PyVLM
Vortex Lattice Method library written in Python
ziliHarvey/CNN-for-Airfoil
CNN for airfoil lift-to-drag-ratio prediction
nathanrooy/BlenderFOAM
Fluid based shape optimization with Blender and OpenFOAM
usuaero/MachLine
A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
ashwinvis/caeroc
☴🖩 Compressible Aerodynamics Calculator for Python
geoffreynyaga/Kenya-One-Project
Aircraft Conceptual Design Software
partmor/ezaero
ezaero - Easy aerodynamics in Python :airplane:
ZeeshanIqbalKhan/AirfoilANN
Official repository of paper, entitled "Airfoil’s Aerodynamic Coefficients Prediction using Artificial Neural Network".
byuflowlab/FLOWPanel.jl
Three-dimensional panel method for low-speed aerodynamics
juri117/cfd-bwb-airfoil-optimizer
optimizes an Airfoil for a blended wing body using cfd analysis with su2 and optimization by openMdao
bernhardpg/babyshark_vtol_model
Full dynamic model for the Babyshark 260 VTOL UAV.
DhyeyR-007/Planar-Endoatmospheric-Missile-Guidance
Developed a missile guidance and ballistic control system for autonomous mid-air and surface-to-air target chase and interception