Computational aeroacoustic modelling using hybrid RANS/LES methods with modified acoustic analogies
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 by turbulence are computed as well as the correspondin...
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| Format: | Dissertation |
| Language: | English |
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University of Cape Town
2017
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| Online Access: | http://hdl.handle.net/11427/25388 |