| タイトル | Effect of wall suction on performance of a short annular diffuser at inlet Mach numbers up to 0.5 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750024928 |
| 著者（英） | Juhasz, A. J. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1975-10-01 |
| 言語 | eng |
| 内容記述 | A short annular diffuser equipped with wall bleed (suction)capability was evaluated at inlet Mach numbers of 0.186 to 0.5. The diffuser had an area ratio of 4.0 and a length-to-inlet height ratio of 1.6. Test results show that the exit velocity profiles, typical of annular jet flow without suction, could be considerably flattened by application of wall suction. This improved performance was also reflected in diffuser effectiveness (static-pressure recovery) and total-pressure loss results. At the inlet Mach number of 0.5 diffuser static-pressure recovery is equal to or better than at lower inlet Mach numbers for comparable suction rates. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 75N33001
NASA-TM-X-3302
E-8393 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/188533 |
