peterdsharpe / NeuralFoil
NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
☆140Updated last month
Related projects ⓘ
Alternatives and complementary repositories for NeuralFoil
- Blade Element Momentum Method for Propellers and Turbines☆59Updated 2 months ago
- An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy☆265Updated this week
- CEASIOMpy is a Python conceptual aircraft design environment☆77Updated last week
- Meshless large eddy simulation through the reformulated vortex particle method☆76Updated this week
- MACH: MDO of Aircraft Configurations with High fidelity☆116Updated this week
- Stripped down version of XFOIL as compiled python module☆88Updated 3 years ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆128Updated last week
- Multiphysics with OpenMDAO☆49Updated 3 months ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆195Updated 3 months ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆58Updated 2 years ago
- Source and vortex panel method codes referenced in my YouTube videos.☆87Updated 4 years ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆54Updated this week
- DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization☆211Updated last week
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆38Updated 2 years ago
- Optimization of an airfoil through a genetic algorithm.☆13Updated 2 years ago
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- NASA's aircraft analysis, design, and optimization tool☆142Updated this week
- The Python XFOIL optimization toolbox can be used to optimize airfoils for a specific operating range, and might be useful to you for its…☆39Updated 7 years ago
- Experiment code associated with our paper: "Aerodynamic Design Optimization and Shape Exploration using Generative Adversarial Networks"☆62Updated 5 months ago
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆40Updated 4 years ago
- A python based blade parametrization tool☆50Updated 3 months ago
- A python library for generating PDF XDSM diagrams.☆59Updated last year
- ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.☆229Updated this week
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆36Updated 4 months ago
- A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superli…☆45Updated 10 months ago
- Python interface for XFOIL. The objective of this library is to be able to be able to call XFOIL from Python iteratively for any simulati…☆66Updated 3 years ago
- PyAero is an open-source airfoil contour analysis and CFD meshing tool.☆174Updated this week
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆20Updated 2 months ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆84Updated 2 months ago
- Surface and foil modeling via CST method☆19Updated 3 weeks ago