Assessment of CFD broadband noise predictions on a rod-airfoil benchmark computation

Marc C. Jacob, M. Ciardi, L. Gamet, B. Greschner, Y. J. Moon, I. Vallet

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

15 Citations (Scopus)

Abstract

This paper presents a selection of acoustic far field, unsteady aerodynamic and mean flow results obtained from a variety of unsteady codes on a low Mach rod-airfoil test case. These codes are all applicable to complex geometries such as encountered in turbo engines. Therefore the present computations can be regarded as an evaluation of their capability to predict turbomachinery broadband noise. This quite unique benchmarking work of turbomachinery noise prediction tools has mainly been achieved within the framework of the European Project PROBAND, but some of the results where also obtained by an academic cooperation with a Korean partner.

Original languageEnglish
Title of host publication14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
Publication statusPublished - 2008
Event14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference) - Vancouver, BC, Canada
Duration: 2008 May 52008 May 7

Publication series

Name14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)

Other

Other14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
CountryCanada
CityVancouver, BC
Period08/5/508/5/7

ASJC Scopus subject areas

  • Engineering(all)

Fingerprint Dive into the research topics of 'Assessment of CFD broadband noise predictions on a rod-airfoil benchmark computation'. Together they form a unique fingerprint.

  • Cite this

    Jacob, M. C., Ciardi, M., Gamet, L., Greschner, B., Moon, Y. J., & Vallet, I. (2008). Assessment of CFD broadband noise predictions on a rod-airfoil benchmark computation. In 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference) [2008-2899] (14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)).