Automated multi-fidelity aerodynamic design pipeline for a High-Lift STOL wing. Integrates Python (AeroSandbox) for parametric optimization, OpenVSP for 3D sizing, and Ansys Fluent (RANS) for high-fidelity physics validation.
A plugin-based desktop application for parametric UAV design and analysis.
An AI-powered surrogate modeling tool for aerodynamic airfoil optimization.
Aerospace system identification, model validation & uncertainty quantification in Python. Fit ODE models to flight-test data with error bars, Kalman filtering, Bayesian inference, optimal experiment design, and JSBSim/RocketPy/AeroSandbox adapters, what the data says the vehicle really is.
Robust multi-objective low-Re airfoil design with AeroSandbox + NeuralFoil, and a 55-airfoil wind-tunnel benchmark of NeuralFoil below Re = 500k
To associate your repository with the aerosandbox topic, visit your repo's landing page and select "manage topics."