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Multiphysics Integrated Computational Project

Example of FE solvers using the amfe library

Source-Doublet Panel Method

Unsteady Panel Method

Build VTK 7 on recent systems

This project has received funding from the European Union’s Horizon Europe Framework Programme under grant agreement No. 101056682 for the project “DIgital DEsign strategies to certify and mAnufacture Robust cOmposite sTructures (DIDEAROT)”. The contents of this publication are the sole responsibility of ULiege and do not necessarily reflect the opinion of the European Union. Neither the European Union nor the granting authority can be held responsible for them.

RAPTOR - Rapid Aircraft Preliminary Optimization & Refinement is a python tool used to perform analysis and optimization at the preliminary stage of aircraft design.

Source-Doublet Panel Method

Native solid (RBM) solver for CUPyDO