| タイトル | Performance of high-area-ratio annular dump diffuser using suction-stabilized-vortex flow control |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770017196 |
| 著者（英） | Smith, J. M.; Juhasz, A. J. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1977-05-01 |
| 言語 | eng |
| 内容記述 | A short annular dump diffuser having a geometry conductive to formation of suction stabilized toroidal vortices in the region of abrupt area change was tested. The overall diffuser area ratio was 4.0 and the length to inlet height ratio was 2.0. Performance data were obtained at near ambient temperature and pressure for inlet Mach numbers of 0.18 and 0.30 with suction rates ranging from 0 to 18 percent of total inlet mass flowrate. Results show that the exit velocity profile could be readily biased toward either wall by adjustment of inner and outer wall suction rates. Symmetric exit velocity profiles were inherently unstable with a tendency to revert to a hub or tip bias. Diffuser effectiveness was increased from about 38 percent without suction to over 85 percent at a total suction rate of 10 to 12 percent. At the same time diffuser total pressure loss was reduced from 3.1 percent to 1.1 percent at an inlet Mach number of 0.3. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 77N24140
E-9011
NASA-TM-X-3535 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/182286 |
