Towards the Effect of the Fluid Ftructure Coupling on the Aeroacoustic Instabilities of Solid Rocket Motors
Résumé
The industrial optimization needs nowadays the treatment of coupled phenomena such as aero-thermal or aero-elasticity. The following paper presents the construction and validation of a coupled software assembly, through the realization of simple test cases with a known analytical solution, with the aim to subsequently use it to solve an industrial configuration coming from the solid propulsion.
Domaines
Mécanique [physics.med-ph]Origine | Fichiers produits par l'(les) auteur(s) |
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