cfmesh

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).

CR25 SpaceConcordia 2025 solid rocketry project: a non-ordinary transition rocket due to new design required in-depth analysis. CFD simulation using OpenFOAM had been conducted to analyze aerodynamic forces on the airframe in different Angle of Attacks and Speeds

cfMesh port for OpenFOAM Foundation v13 with boundary layer robustness improvements. Tested on NASA Rotor 37.