An investigation of the noise field from a small jet and methods for its reduction.

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dc.creator Westley, R.
dc.creator Lilley, G. M.
dc.date 2006-01-26T12:17:51Z
dc.date 2006-01-26T12:17:51Z
dc.date 1952-01
dc.date.accessioned 2022-05-09T10:17:10Z
dc.date.available 2022-05-09T10:17:10Z
dc.identifier http://hdl.handle.net/1826/987
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826/987
dc.description Sound measurements have been made on the noise from the jet of a one inch diameter convergent nozzle at atmospheric temperature and at speeds above and below choking. The noise level and spectrum have been investigated in both the near and distant fields. The results agree in some measure with the predictions of the Lighthill theory, that the elementary sound radiator is an acoustic quadrupole. The agreement is more marked if attention is confined to the higher frequencies. Simple empirical formulae are derived giving the overall sound intensity and frequency spectrum in terms of the position relative to the jet, the stagnation pressure excess over the atmospheric pressure, and the frequency. The results of tests on various noise reduction devices are discussed. These tests indicate promising lines of investigation. The maximum reduction in total noise level was about 10 db.
dc.format 1982 bytes
dc.format 12190796 bytes
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dc.format application/pdf
dc.language en
dc.publisher College of Aeronautics, Cranfield.
dc.relation College Report
dc.relation 53
dc.relation CoA/R;53
dc.title An investigation of the noise field from a small jet and methods for its reduction.
dc.type Report


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