Ales Janka
scientific computing, mathematical modellingOptimisation de forme d’un avion supersonique
Adaptive finite elements
Supersonic flow around the space shuttle:
an insufficient discretisation of physical
laws has been automatically detected by an a-posteriori error indicator and improved.
Shape optimization of magnetic coils
Having parameterized the original shape, we look for the optimal values of the shape parameters. The objective is to produce magnetic
fi elds as homogeneous as possible, while satisfying thermal (cooling)
and mechanical (structural) constraints.