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Effect of Cavity Flow on High Speed Train Pantograph Aerodynamic Noise

机译:腔流量对高速列车底弓气动噪声的影响

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For high-speed trains the aerodynamic noise becomes important for speeds over about 300 km/h. The pantograph is mounted on the train roof, often in a shallow cavity. It is an important source of high-speed train noise because of its elevated position, especially in the presence of noise barriers which shield sources that are lower on the train. In this paper, the flow features and noise sources of a high-speed train pantograph and its recess are numerically investigated for a speed of 300 km/h. The geometry of the pantograph recess is simplified as a 'closed' rectangular cavity and two pantographs (the lower part of a raised one and a full retracted one) are included that are based on a DSA 350 pantograph. To resolve the details of the turbulent flow structures and hence enable accurate noise predictions, the Improved Delayed Detached-Eddy Simulation (IDDES) approach is used to model the flow field. The Ffowcs Williams & Hawkings aeroacoustics model is employed for far-field acoustic calculations based on noise sources on the solid surfaces only, due to low Mach number of the flow. In comparison with the same cavity without pantographs, the flow around the cavity shows slightly different characteristics when the pantographs are placed in the cavity. Strengths of vortices on downstream of the cavity is reduced slightly due to interaction between cavity flow and pantographs. This study indicates that the main noise sources are from the raised pantograph, and the panhead of the retracted pantograph as shear layers impinge on them. The cavity trailing edge also generates significant noise. The far-field noise is found to be broadband. The directivity of the noise radiated from pantographs and cavity is also obtained.
机译:对于高速列车,空气动力学噪声对于超过约300公里/小时的速度变得重要。电机安装在火车屋顶上,通常在浅腔内。它是高速列车噪音的重要来源,因为其位置升高,特别是在存在屏蔽火车上的屏蔽源的噪声屏障中。在本文中,高速列车映射仪及其凹槽的流量特征和噪声源以300 km / h的速度进行了数控研究。包括基于DSA 350 Pantograph的映射仪凹槽的几何形状被简化为“闭合”的矩形腔和两个受限仪(凸起的一个和完全缩回的缩回)。要解决的紊流结构的细节,并因此使准确的噪声预测,改进的延迟独立式涡模拟(IDDES)方法被用于流场进行建模。 FFOWS Williams&Hawkings气容器模型仅用于基于固体表面上的噪声源的远场声学计算,由于流量的低马赫数。与没有受到限子仪的相同腔体相比,当放置在腔体中时,腔周围的流动显示出略微不同的特性。由于腔流量和受电弓之间的相互作用,腔在腔下游的涡流的强度减小。本研究表明,主要噪声源来自凸起的受限仪,缩回的电压仪的平底头作为剪切层撞击它们。腔后缘也产生显着的噪音。发现远场噪声是宽带。还获得了从Pantographs和腔辐射的噪声的方向性。

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