Some thoughts on a proposed in-flight experiment to study the effect of external noise on a swept laminarised wing
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Hyde, D.
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Abstract
A 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.