Journal
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW
Volume 30, Issue 6, Pages 1067-1079Publisher
ELSEVIER SCIENCE INC
DOI: 10.1016/j.ijheatfluidflow.2009.05.002
Keywords
Reynolds-averaged Navier-Stokes equations; Implicit large-eddy simulation; Jet noise; Chevron nozzle; Ffowcs Williams-Hawkings integral
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Funding
- UK Engineering and Physical Sciences Research Council (EPSRC) [GR/T06629/01]
- Royal Society Industry Fellowship Scheme
- EPSRC [EP/F005954/1] Funding Source: UKRI
- Engineering and Physical Sciences Research Council [GR/T06629/01, EP/F005954/1] Funding Source: researchfish
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Hybrid large-eddy type simulations for chevron nozzle jet flows are performed at Mach 0.9 and Re = 1.03 x 10(6). Without using any subgrid scale model (SGS), the numerical approach applied in the present study is essentially implicit large-eddy simulation (ILES). However, a Reynolds-averaged Navier-Stokes (RANS) solution is patched into the near wall region. This makes the overall solution strategy hybrid RANS-ILES. The disparate turbulence length scales, implied by these different modeling approaches, are matched using a Hamilton-Jacobi equation. The complex geometry features of the chevron nozzles are fully meshed. With numerical fidelity in mind, high quality, hexahedral multi-block meshes of 12.5 x 10(6) cells are used. Despite the modest meshes, the novel RANS-ILES approach shows encouraging performance. 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. Encouraging agreement of the predicted far-field sound directivity and spectra with measurements is obtained. (C) 2009 Elsevier Inc. All rights reserved.
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