| タイトル | Aerodynamic performance of flared fan nozzles used as inlets |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760013055 |
| 著者（英） | Kelm, G. G.; Keith, T. G.; Dietrich, D. A. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1976-03-01 |
| 言語 | eng |
| 内容記述 | Tests were conducted in a low speed wind tunnel to determine the aerodynamic performance of several flared fan nozzles. Each of the flared nozzles was a downstream-facing inlet to a model fan that was used to simulate a variable pitch fan during reverse thrust operation. The total pressure recovery of each of the flared nozzles as well as that of an unflared nozzle and a serrated flare nozzle was obtained for comparison. The aerodynamic performance of a selected flared nozzle was considered in further detail. The nozzle surface pressures for a flared nozzle were also determined. Results indicated that the differences in aerodynamic performance among the nozzles were most apparent at the wind-tunnel-off condition. A nonzero free stream velocity significantly reduced the perforamnce of all the nozzles, and crosswind flow (free stream flow perpendicular to the model axis) further reduced the performance of the nozzles. The unflared nozzle and the serrated flare nozzle had reduced aerodynamic performance compared to a solid surface flared nozzle. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 76N20143
NASA-TM-X-3367
E-8539 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186593 |
