| タイトル | Low-Noise Rotorcraft Blades |
| 著者（英） | Brooks, Thomas F. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1994-11-01 |
| 言語 | eng |
| 内容記述 | Blades of helicopter rotors, tilt rotors, and like reshaped to reduce noise, according to proposal. Planform features combination of rearward and forward sweep. Forward sweep over large outer portion of blade constitutes primary noise-reduction feature. Relieves some of compressive effect in tip region, with consequent reduction of noise from compressive sources. Performance at high advance ratio improved. Cabin vibration and loading noise reduced by load-averaging effect of double-sweep planform. Aft-swept section provides balancing of aerodynamic and other dynamic forces on blade along 1/4-chord line of straight inboard section and along projection of line to outermost blade radius. Possible for hub-hinge forces and moments to remain within practical bounds. Provides stabilizing blade forces and moments to counteract any instability caused by forward sweep. |
| NASA分類 | MECHANICS |
| レポートNO | 94B10643
LAR-14569 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/312957 |
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