An experimental investigation of flow-induced noise mechanism of a flexible flat-plate trailing-edge (Record no. 2555)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 01182nam a22001577a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20160513161100.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 160513b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE | |
| Transcribing agency | National Acoustic Laboratories |
| 245 ## - TITLE STATEMENT | |
| Title | An experimental investigation of flow-induced noise mechanism of a flexible flat-plate trailing-edge |
| 520 3# - SUMMARY, ETC. | |
| Summary, etc | The Trailing-Edge (TE) of aircraft wings generates significant noise which is problematic for communities. This paper investigates a possible noise reduction mechanism by using an airfoil with a flexible TE made from Nylon 6 material. Experiments were carried out in an Anechoic Wind Tunnel (AWT) at low-to-moderate Reynolds number 2.8 x 10,Re,4.3x10, based on the chord length. To this end, two different flexible TE models with different chord-wise lengths are studied and their results are compared with that obtained for the rigid TE models (made of aluminium) at different free-stream velocities. |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Chandrashnata Das....[et.al] |
| 773 0# - HOST ITEM ENTRY | |
| Title | Acoustics 2015 Hunter Valley 15-18 November 2015 |
| 856 ## - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="http://dspace.nal.gov.au/xmlui/bitstream/handle/123456789/359/p23.pdf?sequence=1&isAllowed=y">http://dspace.nal.gov.au/xmlui/bitstream/handle/123456789/359/p23.pdf?sequence=1&isAllowed=y</a> |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Source of classification or shelving scheme | Universal Decimal Classification |
| Koha item type | Journal article |
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