| タイトル | A possible explanation for the present difference between linear noise theory and experimental data for supersonic helical tip speed propellers |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840006806 |
| 著者（英） | Dittmar, J. H. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1983-11-01 |
| 言語 | eng |
| 内容記述 | High speed turboprops are attractive candidates for future aircraft because of their high propulsive efficiency. However, the noise of their propellers may create a cabin environment problem for the aircraft powered by these propellers. The noise of some propeller models was measured, and predictions of the noise using a method based on the Ffowcs Williams-Hawkins equation were made. The predictions and data agree well at lower helical tip Mach numbers but deviate above Mach 1.0. Some possible reasons why the theory does not predict the data and focuses on improvement of the aerodynamic inputs as the most likely remedy are investigated. In particular, it is proposed that an increase in the drag and a decrease in the lift near the tip of the blade where the majority of the noise is generated, is warranted in the input to the theory. |
| NASA分類 | ACOUSTICS |
| レポートNO | 84N14874
NAS 1.15:83467
NASA-TM-83467
E-1781 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/160817 |
