Scale effects on the performance of sawtooth spoilers in transonic rectangular cavity flow

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dc.contributor.author Saddington, A. J.
dc.contributor.author Knowles, Kevin
dc.contributor.author Thangamani, Varun
dc.date.accessioned 2019-11-29T15:36:33Z
dc.date.available 2019-11-29T15:36:33Z
dc.date.issued 2015-12-11
dc.identifier.citation Saddington A, Knowles K, Thangamani V. (2016) Scale effects on the performance of sawtooth spoilers in transonic rectangular cavity flow. Experiments in Fluids, Volume 57, Issue 2, January 2016, Article Number 2 en_UK
dc.identifier.issn 0723-4864
dc.identifier.uri https://doi.org/10.1007/s00348-015-2088-2
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/14785
dc.description.abstract An experimental study was conducted on the effectiveness of sawtooth spoilers at suppressing acoustic tones within a rectangular cavity with a length-to-depth ratio of five and a width-to-depth ratio of two, operating at a freestream Mach number of 0.71. Whereas previous research has focussed on the ratio of spoiler height to boundary-layer thickness (h/δ), this study also considers the effect of the ratio of cavity length to boundary-layer thickness (L/δ). Using a combination of unsteady pressure measurements and particle image velocimetry, it was established that consideration of the magnitude of both parameters is important when designing passive control methods for transonic cavities. A correlation was developed which suggests that in order to suppress fully the cavity tones, a critical spoiler height, h cr, is defined such that h cr/δ = 0.065 ≤ L/δ ≤ 0.082. en_UK
dc.language.iso en en_UK
dc.publisher Springer en_UK
dc.rights Attribution 4.0 International *
dc.rights.uri http://creativecommons.org/licenses/by/4.0/ *
dc.subject Particle Image Velocimetry en_UK
dc.subject Shear Layer en_UK
dc.subject Particle Image Velocimetry Measurement en_UK
dc.subject Broadband Noise en_UK
dc.subject Particle Image Velocimetry Data en_UK
dc.title Scale effects on the performance of sawtooth spoilers in transonic rectangular cavity flow en_UK
dc.type Article en_UK
dc.identifier.cris 4090465


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