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Calcul numérique de la réponse acoustique d'un aubage soumis à un sillage turbulent

Abstract : Noise generation due to the rotor wakes impinging the stator vanes is a dominant turbofan source at approach conditions, and the broadband noise component is significantly contributing to the overall level. A numerical method based on a CAA code solving the Euler equations is developped in this thesis in order to simulate the interaction noise between a turbulent wake and a vane row without geometry restrictions. The upstream turbulent flow is synthesized using a stochastic approach by considering an homogeneous isotropic turbulence spectrum model and a simplified spatial representation of the velocity field. These velocity gusts are injected in the CAA code by implementing a suited boundary condition. The present methodology is first va- lidated against turbulence-flat plate interaction cases, by comparing the numerical predictions to Amiet model solutions. A chaining with an integral formulation is also performed to assess the acoustic far-field. Then, the method is used to estimate the acoustic response of an isolated airfoil with a wavy leading egde, designed and tested in ISVR wind tunnel in the framework of European FLOCON project. Finally, the computations are extended to ducted annular grid configurations. After a validation step on single-frequency cases described in a CAA benchmark, broadband noise simulations are performed, firstly on a flat-plate annular grid in a uniform axial flow tested in the LMFA wind tunnel, and then on a more complex configuration related to an unloaded grid in a swirling mean flow proposed by Atassi
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Submitted on : Friday, June 5, 2015 - 3:57:34 PM
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  • HAL Id : tel-01009856, version 2


Vincent Clair. Calcul numérique de la réponse acoustique d'un aubage soumis à un sillage turbulent. Acoustique [physics.class-ph]. Université Claude Bernard - Lyon I, 2013. Français. ⟨NNT : 2013LYO10296⟩. ⟨tel-01009856v2⟩



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