| タイトル | Rotor redesign for a highly loaded 1800 ft/sec tip speed fan. 3: Laser Doppler velocimeter report |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830005857 |
| 著者（英） | Harvey, W. B.; Lee, D.; Williams, K. F.; Hobbs, D. E.; Williams, M. C. |
| 著者所属（英） | United Technologies Corp. |
| 発行日 | 1982-04-01 |
| 言語 | eng |
| 内容記述 | Laser Doppler velocimeter (LDV) techniques were employed for testing a highly loaded, 550 m/sec (1800 ft/sec) tip speed, test fan stage, the objective to provide detailed mapping of the upstream, intrablade, and downstream flowfields of the rotor. Intrablade LDV measurements of velocity and flow angle were obtained along four streamlines passing through the leading edge at 45%, 69%, 85%, and 95% span measured from hub to tip, at 100% of design speed, peak efficiency; 100% speed, near surge; and 95% speed, peak efficiency. At the design point, most passages appeared to have a strong leading edge shock, which moved forward with increasing strength near surge and at part speeds. The flow behind the shock was of a complex mixed subsonic and supersonic form. The intrablade flowfields were found to be significantly nonperiodic at 100% design speed, peak efficiency. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 83N14128
PWA-5523-122
NASA-CR-167954
NAS 1.26:167954 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/164086 |
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