| タイトル | Skin friction on a flat perforated acoustic liner |
| 著者（英） | Brinich, P. F.; Boldman, D. R. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1976-11-01 |
| 言語 | eng |
| 内容記述 | The report concerns the measurement of friction coefficients of a typical perforated acoustic liner installed in the side of a wind tunnel. The results are compared with measured friction coefficients of a smooth hard wall for the same mean flow velocities in a wind tunnel. At a velocity of 61 m/sec, an increase in the local skin coefficient of only a few percent was observed, but at the highest velocity of 213 m/sec an increase of about 20% was obtained. This velocity is a realistic velocity for turbo-machinery components utilizing such liners, so a loss in performance is to be expected. Some tests were also performed to see if changes in the mean boundary layer induced by imposed noise would result in friction increase, but only at low velocity levels was such an increase in friction noted. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 77A13729 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/440111 |
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