Some thoughts on a proposed in-flight experiment to study the effect of external noise on a swept laminarised wing

dc.contributor.authorHyde, D.
dc.date.accessioned2017-07-04T09:08:18Z
dc.date.available2017-07-04T09:08:18Z
dc.date.issued1963-04
dc.description.abstractA transducer-horn arrangement has been suggested as a suitable noise source to be installed in the Lancaster aircraft so that the Handley-Page suction fin could be subjected to large acoustical disturbances. The object of this note is to clarify this proposal with a view to recommending actions to be taken.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/12148
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N-145en_UK
dc.relation.ispartofseries145en_UK
dc.titleSome thoughts on a proposed in-flight experiment to study the effect of external noise on a swept laminarised wingen_UK
dc.typeReporten_UK

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