Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges
Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges
| dc.contributor.author | Dassen, T. | en_US |
| dc.contributor.author | Parchen, R. | en_US |
| dc.contributor.author | Bruggeman, J. | en_US |
| dc.contributor.author | Hagg, F. | en_US |
| dc.date.accessioned | 2017-02-14T10:39:52Z | |
| dc.date.available | 2017-02-14T10:39:52Z | |
| dc.date.issued | 1996 | en_US |
| dc.identifier.other | NLR-TP-1996-350 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/1359 | |
| dc.language.iso | nl | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;1996-350 | en_US |
| dc.subject.other | Aeroacoustics | en_US |
| dc.subject.other | Windtunnels | en_US |
| dc.title | Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges | en_US |
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