Some thoughts on a proposed in-flight experiment to study the effect of external noise on a swept laminarised wing
Date published
1963-04
Free to read from
Authors
Supervisor/s
Journal Title
Journal ISSN
Volume Title
Publisher
College of Aeronautics
Department
Type
Report
ISSN
Format
Citation
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.