Noise prediction for a turbulent jet usi
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E. GrΓΆschel; W. SchrΓΆder; P. Renze; M. Meinke; P. Comte
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Article
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2008
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Elsevier Science
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English
β 894 KB
The acoustic field of a cold single stream jet at Mach number 0.9 and Reynolds number 3600 is determined via computational aeroacoustics (CAA) methods. The jet computation of the acoustical field is performed by two hybrid approaches using a large-eddy simulation (LES) for the flow field and various