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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).
Simulation of transonic flow over a supercritical airfoil using the K-Omega SST Model in OpenFOAM
Demonstration of using transonic to accelerate Python