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Investigation of cavity flows at low and high Reynolds numbers using computational fluid dynamics

机译:利用计算流体动力学研究低雷诺数和高雷诺数下的空腔流动

摘要

Despite the amount of research into the cavity flow problem the prediction of the flow patterns, associated forces and acoustic phenomena remains an unsolved problem. The coupling of the shear layer dynamics, the internal vortical structures and the acoustics of the cavity make it a very complex flow despite the simple geometry. Once doors, stores and release mechanism are added the problem is compounded, thus accurate prediction methods are a necessity. The cavity has been shown to oscillate in different modes depending on the flow conditions and the geometry of the cavity. Two modes of oscillation were examined in detail, these being the wake and shear layer mode, using computational fluid dynamics and experimental data where available. The flow code used is the in-house CFD solver PMB and the experimental data has been provided by DERA. The cavity geometry was for a 1VD=5 cavity with a W/D ratio of 1 for the 3D investigation. For the wake mode the Reynolds number has been varied from 5,000 to 100,000 and the Mach number has been varied from 0.3 to 1.0 in order to examine the effect of changing conditions on this mode of oscillation. The characteristics of this mode of oscillation have been identified and a stable region within the varying Mach and Reynolds numbers has been shown. Outside of this stable region a blended flow has been identified. For the shear layer mode of oscillation the open cavity environment has been examined. This cavity is of great interest as examples of it can be found in current airframes, the H- 111 for example. This flow type is characterised by intense acoustic noise at distinct frequencies which could cause structural fatigue and damage sensitive electronics. However, this cavity type also has a relatively benign pressure distribution along the length of the cavity making it ideal for store separation. The flow cycle predicted shows that the separated shear layer impact on the rear wall generates strong acoustic waves. These waves are further enhanced by the interaction of the wave with the vortices and upstream wall of the cavity. The flow conditions of interest for this case are M=0.85 and Re=6.783 million. A study of the effect of time step, grid refinement and turbulence model has been performed. It has been seen that the density of the grid and the turbulence model chosen must be considered as a pair; if the grid is too fine it may resolve scales being modelled by the turbulence model and result in a double counting of energy resulting in spurious results. One area of cavity studies that has received only sparse investigation is the effect of 3-Dimensionality on the flow. One objective of this work was to try and rectify this. However, it was found that the choice of solver could play a significant role in the accurate prediction of the 3D cavity flow. For cases where the acoustic spectrum is broad, typical URANS codes may have difficulty in predicting these flows. Under such conditions DES or LES would be more appropriate choices. However, when the frequency spectrum is not as spread out URANS can provide good results. This can be seen in the 3D cavity case where doors are present and aligned vertically. The wake mode, while identified in 2D. has received little attention in 3D. It is generally thought that the effect of the third dimension would be to trip the wake mode to shift to another mode of oscillation. This study has shown that this is indeed the case. The flow cycle shown is more reminiscent of the blended flows shown in some 2D cases.
机译:尽管对腔体流动问题进行了大量研究,但是对流型,相关力和声学现象的预测仍然是一个尚未解决的问题。尽管几何形状简单,但剪切层动力学,内部涡旋结构和空腔的声学特性的耦合使它成为非常复杂的流动。一旦添加了门,存储和释放机制,问题就变得更加复杂,因此必须采用准确的预测方法。已经显示出空腔根据流动条件和空腔的几何形状以不同的模式振荡。使用计算流体动力学和实验数据,详细检查了两种振荡模式,即尾流和剪切层模式。所使用的流程代码是内部CFD求解器PMB,实验数据由DERA提供。腔的几何形状用于1VD = 5的腔,W / D比率为1进行3D研究。对于唤醒模式,雷诺数已从5,000更改为100,000,马赫数已从0.3更改为1.0,以检查变化的条件对该振荡模式的影响。已经确定了这种振荡模式的特征,并显示了变化的马赫数和雷诺数内的稳定区域。在该稳定区域之外,已经确定了混合流。对于振荡的剪切层模式,已经研究了开放腔环境。该腔非常有趣,因为可以在当前的机体(例如H-111)中找到它的示例。这种流动类型的特点是在不同的频率产生强烈的声噪声,这可能会导致结构疲劳并损坏敏感的电子设备。但是,这种空腔类型沿空腔的长度方向也具有相对良好的压力分布,因此非常适合存储分离。预测的流动周期表明,分离的剪切层撞击后壁会产生强烈的声波。这些波通过波与涡旋和空腔上游壁的相互作用而进一步增强。在这种情况下,感兴趣的流动条件为M = 0.85和Re = 678.3万。研究了时间步长,网格细化和湍流模型的影响。已经看到,网格的密度和选择的湍流模型必须被视为一对。如果网格太细,则可能会解析由湍流模型建模的比例,并导致对能量的重复计算,从而导致虚假结果。仅接受稀疏研究的腔研究领域之一是三维对流动的影响。这项工作的一个目标是尝试对此进行纠正。但是,发现求解器的选择可能在3D腔流的准确预测中起重要作用。对于声谱较宽的情况,典型的URANS代码可能难以预测这些流量。在这种情况下,DES或LES将是更合适的选择。但是,当频谱不那么分散时,URANS可以提供​​良好的结果。这可以在3D腔体情况下看到,其中存在门并垂直对齐。唤醒模式,以2D模式识别。在3D中几乎没有受到关注。通常认为,三维的作用是使唤醒模式跳闸,以转换为另一种振荡模式。这项研究表明确实如此。所示的流动循环更让人联想到某些2D情况下显示的混合流动。

著录项

  • 作者

    Lawrie David;

  • 作者单位
  • 年度 2004
  • 总页数
  • 原文格式 PDF
  • 正文语种 English
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