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Please use this identifier to cite or link to this item: http://dspace.lib.cranfield.ac.uk/handle/1826/3940

Document Type: Conference paper
Title: Computational aeroacoustic study of a landing gear
Authors: Khanal, B.
Knowles, K.
Saddington, Alistair J.
Obayashi, S.
Issue Date: 2009
Abstract: Computational study of a single wheel landing gear con guration was completed to understand the noise source and it's nature. The ow eld visualisation showed the present of large structural shedding in the wake side of the the landing gear wheel. These large structures were responsible for the low frequency noise. Spectral peaks at frequencies lower than 200 Hz were found to exist from the analysis of the frequency content of the pressure signals at far eld. These low frequency peaks were due to the large structural shedding.
URI: http://dspace.lib.cranfield.ac.uk/handle/1826/3940
Appears in Collections:Staff publications - Cranfield Defence and Security, Shrivenham

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