| タイトル | Wake vortex technology |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780021112 |
| 著者（英） | Barber, M. R.; Dunham, R. E., Jr.; Croom, D. R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1978-01-01 |
| 言語 | eng |
| 内容記述 | A brief overview of the highlights of NASA's wake vortex minimization program is presented. The significant results of this program are summarized as follows: (1) it is technically feasible to reduce significantly the rolling upset created on a trailing aircraft; (2) the basic principles or methods by which reduction in the vortex strength can be achieved have been identified; and (3) an analytical capability for investigating aircraft vortex wakes has been developed. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 78N29055 |
| 権利 | No Copyright |
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