aiaa_final_draft_2-5-2016.pdf (7.32 MB)
Far-field noise prediction of round and serrated jets with increasingly refined grids
conference contribution
posted on 2016-05-31, 13:32 authored by Matteo Angelino, Hao XiaHao Xia, Miguel Moratilla-Vega, Gary PageGary PageTurbulent jet large-eddy simulations (LES) are performed at Mach 0.9 and Reynolds
number of 106. For subgrid scale stress modeling the σ-model is used. Solutions are obtained for a baseline axisymmetric (round) nozzle and a serrated (or chevron) nozzle with high bending and penetration, on grids ranging from 5 to 80 million grid points in order to assess the correlation between coarser and finer grid solutions. Computed mean and second-order fluctuating quantities of the turbulent near field compare favorably with measurements. The radiated far-field sound is predicted using the Ffowcs Williams and Hawkings (FW-H) surface integral method. Remarkable agreement of the predicted farfield sound directivity and spectra with measurements is obtained. A preliminary discussion is presented on the correlation and possible combination of multiple spectra from different grids.
Funding
This work is financially supported by UK Engineering and Physical Sciences Research Council (EPSRC) under grant number EP/M01391X/1
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Published in
22nd AIAA/CEAS Aeroacoustics ConferenceCitation
ANGELINO, M. ...et al., 2016. Far-field noise prediction of round and serrated jets with increasingly refined grids. Presented at the 22nd AIAA/CEAS Aeroacoustics Conference, Lyon, France 30th May- 1st June.Publisher
© AIAAVersion
- AM (Accepted Manuscript)
Publisher statement
This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/Acceptance date
2016-02-02Publication date
2016Notes
This paper was presented at the 22nd AIAA/CEAS Aeroacoustics Conference and the definitive published version is available at http://dx.doi.org/10.2514/6.2016-3047Publisher version
Language
- en