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SEA analysis in the cabin of a regional turboprop with metamaterial lining panels

机译:具有超材料衬板的区域涡轮螺旋桨飞机机舱的SEA分析

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The main goal of this paper is to evaluate the comfort, and hence the interior sound pressure levels, in the cabin of a regional turboprop with metamaterial lining panels under Turbulent Boundary Layer flow over the fuselage during cruise flight conditions. In the preliminary work phase, the design of metamaterial and a numerical analysis at component level were performed. Than, the CAD model of a fuselage section was created representing the typical features and dimensions of an airplane for regional flights and a Statistical Energy Analysis (SEA) model was built by using Va One software. An investigation on the influence of designed metamaterial on the soundproofing of the cabin was presented. Results reveal a reduction in Sound Pressure Level (SPL) of almost 5 dB with respect to classical materials, in overall the frequency range and for all the cavities analyzed, in the configuration with metamaterial applied as core of the sandwich lining panels.
机译:本文的主要目标是评估在巡航飞行条件下,湍流边界层在机身上方流动时,带有超材料衬里板的区域涡轮螺旋桨飞机机舱的舒适度,从而评估其内部声压水平。在初步工作阶段,进行了超材料的设计和组件级的数值分析。然后,创建了代表部分飞机的典型特征和尺寸的机身截面的CAD模型,并使用Va One软件构建了统计能量分析(SEA)模型。研究了设计的超材料对机舱隔音的影响。结果表明,相对于传统材料,在整个频率范围内,对于所有分析的空腔,在将超材料用作三明治衬板的核心的配置中,声压级(SPL)降低了近5 dB。

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