| タイトル | Potential for Landing Gear Noise Reduction on Advanced Aircraft Configurations |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160009107 |
| 著者（英） | Thomas, Russell H.; Nickol, Craig L.; Guo, Yueping; Burley, Casey L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2016-05-30 |
| 言語 | eng |
| 内容記述 | The potential of significantly reducing aircraft landing gear noise is explored for aircraft configurations with engines installed above the wings or the fuselage. An innovative concept is studied that does not alter the main gear assembly itself but does shorten the main strut and integrates the gear in pods whose interior surfaces are treated with acoustic liner. The concept is meant to achieve maximum noise reduction so that main landing gears can be eliminated as a major source of airframe noise. By applying this concept to an aircraft configuration with 2025 entry-into-service technology levels, it is shown that compared to noise levels of current technology, the main gear noise can be reduced by 10 EPNL dB, bringing the main gear noise close to a floor established by other components such as the nose gear. The assessment of the noise reduction potential accounts for design features for the advanced aircraft configuration and includes the effects of local flow velocity in and around the pods, gear noise reflection from the airframe, and reflection and attenuation from acoustic liner treatment on pod surfaces and doors. A technical roadmap for maturing this concept is discussed, and the possible drag increase at cruise due to the addition of the pods is identified as a challenge, which needs to be quantified and minimized possibly with the combination of detailed design and application of drag reduction technologies. |
| NASA分類 | Acoustics |
| レポートNO | NF1676L-22681 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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