钝体扩散效应的数值研究:气动特性

M. Y. Setiawan, M. Martias, Erzeddin Alwi
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引用次数: 2

摘要

本文主要对靠近自由通道面下游的钝体周围的流动结构进行了数值研究。在高雷诺数条件下(ReH = 2.19 × 106),采用压力系数、阻力系数、升力系数和表面摩擦系数进行了研究。详细地阐述了本研究的一般程序,用于流体计算动力分析的分配。所使用的数值模型是二维RANS模型(稳定雷诺兹平均纳维·斯托克斯),通过给出40米/秒的流速,采用标准k-系数模型。该虚张声势体模型将在背面添加扩压器处理,其结果将与没有添加扩压器的模型进行比较,并在两个模型的前顶部添加圆形。研究发现,加扩压器后的钝体阻力系数比不加扩压器的钝体阻力系数大,可以认为是由于采用的扩压器角度过大导致阻力系数变大。
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NUMERICAL STUDY OF DIFFUSER EFFECT ON BLUFF BODY : AERODYNAMIC CHARACTERISTICS
This study focuses on the numerical study of flow structure analysis around bluff bodies close to the downstream face of the free-channel surface. This was investigated using coefficient pressure, coefficient drag, lift coefficient and skin friction coefficient on high Reynolds number (ReH = 2.19 × 106). The general procedure for this research is formulated in detail for allocations in dynamic analysis of fluid computing. The numerical model used is the 2D RANS model (Steady Reynolds Averaged Navier Stokes) with the standard k-ɛ model by giving a flow rate of 40 m / s. This bluff body model will be given the addition of diffuser treatment on the back where the result will be compared to the model without the addition of diffuser and the addition of round shape on the top front on both models. From the research it was found that the coefficient drag bluff body with the addition of diffuser is bigger than the bluff body without the diffuser, it can be concluded that the diffuser angle used is too big causing the coefficient drag to become bigger.
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