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Étude aéroacoustique de l'interaction orthogonale pale/tourbillon

Abstract : The aeronautics industry focuses on decreasing its ecological footprint and increasing airplanes efficiency. One way for this is to design more efficient motors, like CROR, for Counter Rotating Open Rotor. This engine, also called propfan, is quite close to a turbofan, but with a pair of counter rotating propellers instead of ducted fan, which increase its yield. The efficiency is about 30 % higher than a turbofan of equal power, but it generates a lot of noise.This noise has several causes, the main one at low speed (typical takeoff or landing situation), is due to the interaction between propellers. The higher contribution to this interaction is the interaction between rear blades and tip vortexes generated by front blades. The noise generation process of this interaction is complex. It has been shown in previous studies at Onera that vortex kind plays an important role on the generated noise.The goal of this thesis is to identify and classify the influent parameters of this interaction on the noise generation, especially the blade geometry and the vortex properties, and then, to find a silent configuration.To this aim, a parametric study is set up. This study is based on a numerical approach and uses the Cassiopée and Kim computational softwares, developed at Onera. Physical models uses Euler unsteady equations, in their three dimensional and compressible expression, for the CFD and Ffowcs-Williams and Hawkings equations, in their rotating solid surface expression, for the CAA. Simulations are run on high orders schemes and use the Chimera method. Analyses are based on both close field fluid dynamics and far field acoustics.With the results of this parametric study, silent and optimal blades design criteria will be find out.Then, with these criteria, it will be possible to design CROR blades which are aeroacoustically efficient as well as aerodynamically efficient. The outcomes of this thesis are not limited to CROR situation only: any configuration where a blade crosses a vortex orthogonally can benefits from this study, by instance the interaction in a helicopter between the main rotor flow and the tail rotor blades.
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Submitted on : Tuesday, October 2, 2018 - 1:51:09 PM
Last modification on : Wednesday, September 28, 2022 - 5:59:39 AM
Long-term archiving on: : Thursday, January 3, 2019 - 2:34:40 PM


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  • HAL Id : tel-01885907, version 1


Paul Zehner. Étude aéroacoustique de l'interaction orthogonale pale/tourbillon. Acoustique [physics.class-ph]. Ecole nationale supérieure d'arts et métiers - ENSAM, 2018. Français. ⟨NNT : 2018ENAM0005⟩. ⟨tel-01885907⟩



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