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Numerical simulation of single-stream jets from a serrated nozzle
journal contribution
posted on 2023-06-08, 14:31 authored by Hao Xia, Paul G TuckerHybrid large-eddy type simulations for cold jet flows from a serrated nozzle are performed at an acoustic Mach number Ma_ac ?=?0.9 and Re?=?1.03×106. Since the solver being used tends towards having dissipative qualities, the subgrid scale (SGS) model is omitted, giving a numerical type LES (NLES) or implicit LES (ILES) reminiscent procedure. To overcome near wall streak resolution problems a near wall RANS (Reynolds averaged Navier-Stokes) model is smoothly blended to the LES making a hybrid RANS-ILES. The geometric complexity of the serrated nozzle is fully considered without simplification or emulation. An improved but still modest hexahedral multi-block grid with circa 20 million grid points (with respect to 12.5 million in Xia et al., Int J Heat Fluid Flow 30:1067–1079, 2009) is used. Despite the modest grid size, encouraging and improved results are obtained. Directly resolved mean and second-order fluctuating quantities along the jet centerline and in the jet shear layer compare favorably with measurements. The radiated far-field sound predicted using the Ffowcs Williams and Hawkings (FW-H) surface integral method shows good agreement with the measurements in directivity and sound spectra.
History
Publication status
- Published
Journal
Flow, Turbulence and CombustionISSN
1386-6184Publisher
Springer VerlagExternal DOI
Issue
1-2Volume
88Page range
3-18Department affiliated with
- Engineering and Design Publications
Full text available
- No
Peer reviewed?
- Yes
Legacy Posted Date
2013-03-04Usage metrics
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