| タイトル | Design of Quiet Rotorcraft Approach Trajectories |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090026010 |
| 著者（英） | Marcolini, Michael A.; Padula, Sharon L.; Boyd, D. Douglas, Jr.; Burley, Casey L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2009-06-01 |
| 言語 | eng |
| 内容記述 | A optimization procedure for identifying quiet rotorcraft approach trajectories is proposed and demonstrated. The procedure employs a multi-objective genetic algorithm in order to reduce noise and create approach paths that will be acceptable to pilots and passengers. The concept is demonstrated by application to two different helicopters. The optimized paths are compared with one another and to a standard 6-deg approach path. The two demonstration cases validate the optimization procedure but highlight the need for improved noise prediction techniques and for additional rotorcraft acoustic data sets. |
| NASA分類 | Acoustics |
| レポートNO | NASA/TM-2009-215771
LF99-9005
L-19701 |
| 権利 | No Copyright |
