| タイトル | Preliminary results of simulated vortex encounters by a twin-engine, commercial aircraft during final landing approach |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800017786 |
| 著者（英） | Holbrook, G. T.; Hastings, E. C., Jr.; Keyser, G. L., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1980-05-01 |
| 言語 | eng |
| 内容記述 | Piloted simulations of encounters with vortices of various ages and degrees of attenuation were performed with the Visual Motion Simulator. In the simulations, a twin engine, commercial transport on final approach, encountered the modeled vortices of a four engine, wide body, commercial transport. The data show the effect of vortex age and attenuation on the severity of the initial upset, as well as the effect of the vortex encounters on the landing capability. |
| NASA分類 | AIR TRANSPORTATION AND SAFETY |
| レポートNO | 80N26285
NASA-TM-81782 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/172222 |
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