| タイトル | HSCT noise reduction technology development at GE Aircraft Engines |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940028960 |
| 著者（英） | Majjigi, Rudramuni K. |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1992-04-01 |
| 言語 | eng |
| 内容記述 | The topics covered include the following: High Speed Civil Transport (HSCT) exhaust nozzle design approaches; GE aircraft engine (GEAE) HSCT acoustics research; 2DCD non-IVP suppressor ejector; key sensitivities from reference aircraft; acoustic experiments; aero-mixing experimental set-up; fluid shield nozzle; HSCT Mach 2.4 flade nozzle; noise prediction; nozzle concept for GE/Boeing joint test; scale model hot core flow path modified to prevent hub-choking CFL3-D solution; HSCT exhaust nozzle status; and key acoustic technology issues for HSCT's. |
| NASA分類 | ACOUSTICS |
| レポートNO | 94N33466 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/111985 |
