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MAS-DAAA-2025-32

Implementation and analysis of the aeroelastic coupling for aeronautical slender structures with rapid methods

Meudon

Thématique(s):

Aeroelasticity

Reduced order models

vortex particle method (VPM)

Aeroelastic interactions

Large aspect ratio wings

Open Rotor And Stator (ORAS)

À Pourvoir

MAS:

dsd-mas@onera.fr

Contact:

mikel.balmaseda@onera.fr