| dc.creator | Hyde, D. | |
| dc.date | 2017-07-04T09:08:18Z | |
| dc.date | 2017-07-04T09:08:18Z | |
| dc.date | 1963-04 | |
| dc.date.accessioned | 2022-05-09T10:07:12Z | |
| dc.date.available | 2022-05-09T10:07:12Z | |
| dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/12148 | |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4511 | |
| dc.description | 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. | |
| dc.language | en | |
| dc.publisher | College of Aeronautics | |
| dc.relation | CoA/N-145 | |
| dc.relation | 145 | |
| dc.title | Some thoughts on a proposed in-flight experiment to study the effect of external noise on a swept laminarised wing | |
| dc.type | Report |
| Files | Size | Format | View |
|---|---|---|---|
| COA_N_145_1963.pdf | 654.9Kb | application/pdf |
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