| タイトル | An analytical and experimental comparison of the flow field of an advanced swept turboprop |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830005790 |
| 著者（英） | Chang, L. K.; Bober, L. J.; Neumann, H. E.; Serafini, J. S. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1983-01-01 |
| 言語 | eng |
| 内容記述 | An argon ion laser velocimeter with four beams was used to measure the detailed flow-field of an advanced eight blade propeller with 45% of tip sweep in an 8x6 foot supersonic wind tunnel. Data were obtained at a free stream Mach number of 0.8, the design advance ratio of 3.06 and a power coefficient of 1.8. Data are presented for inlet flow, exit flow, flow within the blades and flow slightly outside the blade tips. The data are compared to a lifting line theory. In general, the results of the comparison are considered favorable. |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 83N14061
E-1481
NASA-TM-83037
AIAA PAPER 83-0189
NAS 1.15:83037 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/164106 |
