Université de Lyon (92 rue Pasteur - CS 30122, 69361 Lyon Cedex 07 - France)
Abstract : Turbulent flow interactions with the outlet guide vanes are known to be mainly contributing to broadband noise emission of aeroengines at approach conditions. This paper presents a 3D CAA hybrid method aiming at simulating the aeroacoustic response of an annular cascade impacted by a prescribed homogeneous isotropic turbulent flow. It is based on a time-domain Euler solver coupled to a synthetic turbulence model implemented in the code by means of a suited inflow boundary condition proposed by Tam. The fluctuating pressure over the airfoil surface provided by CAA is used as an input to a FWH integral to calculate the radiated sound field. The method is first validated against an academic CAA benchmark in the case of a harmonic gust interacting with an annular flat plate cascade. Then, simulations are applied to turbulence-cascade interactions for annular configurations, in uniform and swirling mean flows, and numerical results in terms of sound power spectra in the outlet duct are compared to semi-analytical and numerical solutions, and to an available experiment.
https://hal-onera.archives-ouvertes.fr/hal-01067864
Contributeur : Véronique Soullier
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Soumis le : mercredi 24 septembre 2014 - 11:28:46
Dernière modification le : mercredi 28 mars 2018 - 14:06:02
Document(s) archivé(s) le : vendredi 14 avril 2017 - 14:13:54
V. Clair, C. Polacsek, T. Le Garrec, M.C. Jacob. Numerical Predictions of Turbulence-Cascade Interaction Noise Using CAA with a Stochastic Model. 20th AIAA/CEAS Aeroacoustics Conference, Jun 2014, ATLANTA, United States. 〈hal-01067864〉
