| タイトル | Flight test investigation of the vortex wake characteristics behind a Boeing 727 during two-segment and normal ILS approaches (A joint NASA/FAA report) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750009268 |
| 著者（英） | Tymczyszyn, J. J.; Jacobsen, R. A.; Garodz, L. J.; Stinnett, G. W., Jr.; Mcmurtry, T. C.; Barber, M. R.; Smith, H. J.; Robinson, G. H.; Devereaux, R. L.; Kurkowski, R. L. |
| 著者所属（英） | NASA Flight Research Center |
| 発行日 | 1975-01-01 |
| 言語 | eng |
| 内容記述 | Flight tests were performed to evaluate the vortex wake characteristics of a Boeing 727 aircraft during conventional and two-segment instrument landing approaches. Smoke generators were used for vortex marking. The vortex was intentionally intercepted by a Lear Jet and a Piper Comanche aircraft. The vortex location during landing approach was measured using a system of phototheodolites. The tests showed that at a given separation distance there are no readily apparent differences in the upsets resulting from deliberate vortex encounters during the two types of approaches. The effect of the aircraft configuration on the extent and severity of the vortices is discussed. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 75N17340
FAA-NA-75-151
NASA-TM-X-62398 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/191063 |
