| タイトル | Some considerations on the integration of engine nacelles into low-boom aircraft concepts |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920076753 |
| 著者（英） | Mack, Robert J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1992-10-01 |
| 言語 | eng |
| 内容記述 | A study of wind-tunnel data has shown why unexpected strong shock waves appeared in wind tunnel pressure signatures of two low-boom models, and has indicated that changes to the current methods for analyzing and designing low-boom aircraft are needed. The discussion provided corrections for the interface lift code, and suggested methods of treatment for the equivalent areas of the aircraft, especially the nacelles and the interference lift, which were to be used in the aircraft design and the sonic boom analysis. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 92X10707 |
| 権利 | No Copyright |
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