| タイトル | Quiet Honeycomb Panels |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100017150 |
| 著者（英） | Klos, Jacob; Palumbo, Daniel L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2010-01-01 |
| 言語 | eng |
| 内容記述 | Sandwich honeycomb composite panels are lightweight and strong, and, therefore, provide a reasonable alternative to the aluminum ring frame/stringer architecture currently used for most aircraft airframes. The drawback to honeycomb panels is that they radiate noise into the aircraft cabin veil- efficiently provoking the need for additional sound treatment which adds weight and reduces the material's cost advantage. A series of honeycomb panels was made -hick incorporated different design strategies aimed at reducing the honeycomb panels' radiation efficiency while at the same time maintaining their strength. The majority of the designs were centered around the concept of creating areas of reduced stiffness in the panel by adding voids and recesses to the core. The effort culminated with a reinforced/recessed panel which had 6 dB higher transmission loss than the baseline solid core panel while maintaining comparable strength. |
| NASA分類 | Composite Materials |
| レポートNO | NF1676L-9856 |
| 権利 | No Copyright |
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