This project provides a complete toolchain for evaluating different rocket geometries at subsonic, transonic, and supersonic regimes. The work contained in this repository is part of a student project carried out at the Technical University of Munich (TUM) under the Master of Science (M.Sc) in Aerospace (year 2023).

An object-oriented Python 3 GUI and API for single- and multi-element parametric airfoil design, analysis, and optimization

Simulation of transonic flow over a supercritical airfoil using the K-Omega SST Model in OpenFOAM

Demonstration of using transonic to accelerate Python

Safety-supervised world models and model-based reinforcement learning for transonic and supersonic autonomous flight control, simulation, and runtime assurance.