| タイトル | Turbulence characteristics of compressor discharge flows |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790016824 |
| 著者（英） | Grant, H. P. |
| 著者所属（英） | Pratt and Whitney Aircraft Group |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | Turbulence measurements were conducted in a large gas turbine engine (JT9D) at the entrance to the diffuser duct, joining the compressor discharge to the combustor inlet. Hot film probe and hot wire probe measurements were obtained at temperatures from 450K (350F) (idle) to 608K (635F) (rich approach). At I.D. (25 percent span) and mid-span locations, the turbulence intensity increased slightly from 6 + or - percent at idle condition to 7 or - 1 percent at rich approach. At O.D. (75 percent span) the turbulent intensity increased more rapidly, from 7.5 + or - 0.5 percent at idle to 15 + or - 0.5 percent at rich approach. The spectra showed turbulent energy distributed uniformly over a 0.1 to 5 KHz bandwidth (down 3db) at all operating conditions, corresponding to random turbulence with velocity wave lengths of 2 cm to 1 meter travelling at the mean velocity of 100 m/sec. Tests results are given in tables and graphs. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 79N24995 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/569125 |
