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Kick-off Meeting of the ENOVAL project

Cenaero's Turbomachinery Advanced Aerodynamics team and Turbomachinery Multi-disciplinary Design team will contribute to WP 4.3 of the ENOVAL european project, with the development of a new methodology to assess the flutter stability analysis of a highly loaded compressor. Based on an integration of unsteady CFD with a moderate computational cost thanks to a phase-lagged approach, the ambition of this methodology is to drastically reduce the number of required simulations building upon adaptive sampling techniques. As a result, the flutter boundary shall be accurately predicted through a cost-effective spanning of the multi-dimensional parameter space (mode, nodal diameter, rotational speed and throttling position).
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