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Turbulence Characterization of Large Scale Airflows in an Aircraft Cabin Mockup

机译:飞机机舱模型中大规模气流的湍流特性

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The objective of our paper is to investigate the turbulence characterization of the airflow in an aircraft cabin mockup.Our experimental investigation was conducted in a full scale 7-rows single-aisle aircraft cabin mock-up designed as a generic replica of a section of the Boeing 737-200.The data was collected by using IFA-300 constant-temperature anemometry,which can continuously sense flow velocity and automatically adjust the dynamic response,then accurately measure the flow fluctuating velocity signals.The velocity,turbulent kinetic energy,spectrum analysis and turbulence scales were investigated.We conclude that the air entrainments decayed the velocities faster than the wall shear stress as shown.The time size step of LES should be less than 1/100 s according to our results.The turbulence eddy scales were 4 cm to 10 cm at the measured area.
机译:本文的目的是研究机舱模型中气流的湍流特性。我们的实验研究是在全尺寸的7行单通道飞机机舱模型中进行的,该模型设计为飞机一部分的通用副本。波音737-200。使用IFA-300恒温风速仪收集数据,可以连续感应流速并自动调节动态响应,然后精确测量流速波动信号。速度​​,湍动能,频谱分析我们得出的结论是,空气夹带使速度衰减的速度快于壁切应力,如图所示。根据我们的结果,LES的时间大小步长应小于1/100 s。湍流涡度为4 cm到测量区域的10厘米。

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