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Flow and Acoustics of a Coaxial Nozzle: a Sensitivity Study to the Inlet Boundary Conditions
Aerospace Systems, University of Cincinnati.ORCID iD: 0000-0001-7330-6965
Aerospace Engineering, University of Cincinnati.
Energy Sciences, Lund University.
Energy Sciences, Lund University.
2006 (English)In: 44th AIAA Aerospace Sciences Meeting 2006, 2006, 7375-7393 p.Conference paper, Published paper (Refereed)
Abstract [en]

The jet noise generated by the high velocity hot stream exhausting from a jet engine represents a major component of the aircraft noise. Reductions in jet noise has been achieved by using high bypass turbo-fan engines. To solve numerically this problem the flow and acoustic fields generated by two coaxial jets are considered. Large Eddy Simulation (LES) is used to handle the non-isothermal turbulent flow field, while for the acoustic field a wave equation with source terms provided by the instantaneous LES is employed. The effects of the inlet boundary conditions on the flow and acoustics are assessed in this paper. A comparison of the computed mean flow field and the SPL with experimental data show excellent agreement at distances of over a few jet diameters downstream of the the jet exit plane. In the proximal part the agreement is less good. However, the discrepancy between the simulations and the experiments is less than the corresponding variations due to the uncertainties in the experimental boundary conditions.

Place, publisher, year, edition, pages
2006. 7375-7393 p.
National Category
Fluid Mechanics and Acoustics Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-48037ISBN: 13: 978-1-56347-807-9 (print)OAI: oai:DiVA.org:kth-48037DiVA: diva2:456655
Conference
44th AIAA Aerospace Sciences Meeting 2006. Reno, NV. 9 January 2006 - 12 January 2006
Note
QC 20111117. AIAA 2006-619Available from: 2011-11-15 Created: 2011-11-15 Last updated: 2011-11-17Bibliographically approved

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http://pdf.aiaa.org/preview/CDReadyMASM06_778/PV2006_619.pdf

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Mihaescu, Mihai

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