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- W2316124154 abstract "Aeroacoustic testing in conventional wind-tunnel is difficult and expensive. In this paper an alternative configuration for such tests is proposed in which the model is moved through an anechoic toroidal chamber. Some of the problems which would have to be overcome are discussed and a first attempt is made to quantify the fluid dynamics of such a device, in order to estimate what size it would have to be in order to be effective. The feasibility of using such a device for aeroacoustic testing is at present undecided, as is its competitiveness in comparison with convention methods. Nomenclature d diameter of duct g gravitational acceleration K screen coefficient p pressure r radius of chamber cross-section R radius of toroidal chamber u velocity U f linear velocity of screen Um mean linear velocity of air α Um U f β f K R r ρ air density" @default.
- W2316124154 created "2016-06-24" @default.
- W2316124154 creator A5048412423 @default.
- W2316124154 date "2003-05-12" @default.
- W2316124154 modified "2023-09-27" @default.
- W2316124154 title "The Aeroacoustic Carousel: A Novel Test Facility" @default.
- W2316124154 cites W2026690725 @default.
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- W2316124154 doi "https://doi.org/10.2514/6.2003-3264" @default.
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