External noise level on lancaster PA474

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dc.contributor.authorTrayford, R. S.
dc.date.accessioned2017-06-22T09:18:18Z
dc.date.available2017-06-22T09:18:18Z
dc.date.issued1963-02
dc.description.abstractMeasurements of the external noise level on the Lancaster aircraft PA474 were made at 10,000 feet at two flight speeds for various Merlin engine conditions. In addition the effect on the noise of running one of the Budworth gas turbines, used for the suction wing experiment, was determined. The results show that the maximum sound pressure level found in flight was 124 DB … [cont.].en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/12090
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N-138en_UK
dc.relation.ispartofseries138en_UK
dc.titleExternal noise level on lancaster PA474en_UK
dc.typeReporten_UK

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CoA. Notes (1952-1969)