On some aspects of the noise propagation from supersonic aircraft

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dc.contributor.authorLilley, G. M.
dc.contributor.authorWestley, R.
dc.contributor.authorYates, A. H.
dc.contributor.authorBusing, J. R.
dc.date.accessioned2012-09-12T13:25:04Z
dc.date.available2012-09-12T13:25:04Z
dc.date.issued1953-02
dc.description.abstractThe noise problem associated with an aircraft flying at supersonic speeds is shown to depend primarily on the shock wave pattern formed by the aircraft. The noise intensity received by a ground observer from a supersonic aircraft flying at high as well as low altitudes, is shown to be high although it is of a transient nature. Continues…en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7569
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reportsen_UK
dc.relation.ispartofseries71en_UK
dc.titleOn some aspects of the noise propagation from supersonic aircraften_UK
dc.typeReporten_UK

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