Investigation of the effect of turbulence intensity and nozzle exit boundary layer thickness on stab...
Investigation of the effect of turbulence intensity and nozzle exit boundary layer thickness on stability pattern of subsonic jet
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Villeurbanne: EDP Sciences
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Language
English
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Villeurbanne: EDP Sciences
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In this study, factors affecting the noise generation by instability waves in a subsonic jet with acoustic Mach number of 0.5 are investigated using linear stability analysis. The base flow required for instability analysis is obtained by modeling the jet stream based on the k-ε turbulence model and using the empirical coefficients suggested by Thi...
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Investigation of the effect of turbulence intensity and nozzle exit boundary layer thickness on stability pattern of subsonic jet
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TN_cdi_proquest_journals_2282991131
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https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_proquest_journals_2282991131
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ISSN
2257-7777
E-ISSN
2257-7750
DOI
10.1051/meca/2018041