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Experimental investigation of porous materials for trailing-edge noise reduction

机译:用于后缘降噪的多孔材料的实验研究

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摘要

The introduction of quiet short take-off and landing for civil aircraft operations in close proximity to the population poses important technological challenges. One critical aspect is the realization of extreme lift augmentation at low acoustic emissions. The aircraft concept selected to achieve this goal is a high-lift system equipped with an active flow-control non-slotted flap and a droop nose. For this specific configuration, trailing edge noise becomes a dominant noise source. Porous materials as a passive means for trailing-edge noise reduction are selected and characterized. Results of extensive experimental investigations in the acoustic wind tunnel Braunschweig are presented and discussed to point out the potential and limitations of the selected porous devices. Practical issues related to material manufacturing and integration into the wind tunnel model are addressed. The noise reduction potential of passive porous trailing-edge devices is found to strongly depend on both these aspects. Issues related to the characterization of the porous materials properties are described. Although porous materials are found to be successful at reducing trailing-edge noise emissions, the results indicate that there is still a need for more generic investigations to further clarify the parametric dependencies between noise reduction and material properties.
机译:在靠近人口附近的民用飞机运营的安静短暂起飞和降落造成了重要的技术挑战。一个关键方面是在低声学排放处实现极端升力。选择实现这一目标的飞机概念是一个高升力系统,配备有主动流量控制的非开槽襟翼和下垂鼻子。对于这种特定配置,后缘噪声成为主导噪声源。选择和表征作为用于后缘噪声降低的被动装置的多孔材料。提出和讨论了声学风洞Braunschweig中大量实验研究的结果,以指出所选多孔装置的电位和限制。解决了与物料制造和集成到风洞模型相关的实际问题。发现被动多孔后缘装置的降噪电位强烈取决于这两种方面。描述了与多孔材料性质表征相关的问题。尽管发现多孔材料在减少后缘噪声排放时成功,但结果表明仍然需要更多的通用调查,以进一步阐明降噪和材料特性之间的参数依赖性。

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