Study of the aerodynamics/aeroacoustics of an axial-flow fan: Experimental validation of a LES/LPCE/Brinkman penalization method

Florent Ravelet, Sofiane Khelladi, Hussain Nouri, Farid Bakir, Hoyeon Kim, Youngmin Bae, Young J. Moon

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

The seek for an efficient aerodynamic and aeroacoustic design of axial-flow fans is an important field of investigation for both academic and applied research. Improvements can only be made with a better understanding of the physical mechanisms arising in these machines that combine strong interactions between rotating and non-rotating parts of highly complex geometries. One way is to couple well-suited experimental investigations and innovative computational methods, that overtake the weaknesses of methods based for instance on aeroacoustic analogy. In this paper we study an axial fan using a new numerical method based on LES/LPCE Brinkman Penalization Method. This method is developed in the Department of Mechanical Engineering at Korea University. The experimental tests and validations are performed in the Laboratory of Fluid Dynamics at Arts & Métiers ParisTech in Paris. Detailed analysis of numerical and experimental results are in progress within the two partner teams. In this paper we present preliminary encouraging results.

Original languageEnglish
Title of host publication16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781600867446
DOIs
Publication statusPublished - 2010

Publication series

Name16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)

ASJC Scopus subject areas

  • Aerospace Engineering
  • Acoustics and Ultrasonics

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    Ravelet, F., Khelladi, S., Nouri, H., Bakir, F., Kim, H., Bae, Y., & Moon, Y. J. (2010). Study of the aerodynamics/aeroacoustics of an axial-flow fan: Experimental validation of a LES/LPCE/Brinkman penalization method. In 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference) [2010-3869] (16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2010-3869