Computational Aeroacoustic Modelling using Hybrid RANS‐LES Methods with Modified Acoustic Analogies
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DOI: 10.1002/fld.4990
Abstract: This study considers a numerical approach to identifying noise mechanisms in tandem cylinders to understand aircraft landing gear as a primary contributor to airframe noise during approach and landing. Fluctuations in the flow properties induced… read more here.
Keywords: computational aeroacoustic; hybrid rans; using hybrid; aeroacoustic modelling ... See more keywords