Effect of Flare Geometry on the Flow Field of Radial-Radial Swirlers

Ayşe Bay, Firat Kiyici, M. Perçin
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Abstract

In this study, an experimental investigation is conducted to assess the impact of the flare geometry on the mean flow field generated by radial-radial swirlers. Two-dimensional two-component PIV measurements are performed on the mid-plane of a non-reacting planar combustor test section. Three-dimensional numerical simulations are conducted for selected cases to support experimental observations. In a previous study conducted in the same setup, counter-rotating radial-radial swirlers without flare extension were investigated. In this study, in addition to the previously studied baseline swirler geometry, four different swirlers are investigated with three different flare geometries (a rounded flare geometry with a radius of 4 mm and two chamfered flares at angles of 27.5° and 45°) with the rounded one having both co- and counter-rotating configurations. Analysis of the time-averaged flow fields reveals that there is an increase in radial velocity values and a decrease in axial velocity values as a result of the introduction of the flare geometry, which results in a sudden expansion of the swirling jet. When different flare geometries are compared, almost identical flow fields are observed and the formation of a CRZ is not observed for any geometry that employs a flare geometry. Although the maximum negative axial velocity values decrease for geometries with flare, due to the increase of the recirculation radius, the recirculating mass flow rate is higher than the baseline swirler. On the other hand, the recirculating mass flow rate is higher in the co-rotating swirler configuration due to stronger adverse pressure gradient along the central axis of the jet when compared to counter-rotating configuration. Coherent flow structures are identified by using the snapshot POD method and different mode shapes obtained for swirlers with and without flare geometry are reported. It is shown that the change of the sense of rotation and flare geometry does not bring about any differences in the POD modes and their energy contents for the given swirl number and confinement conditions.
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耀斑几何形状对径向旋流器流场的影响
在本研究中,进行了实验研究,以评估耀斑几何形状对径向旋流器产生的平均流场的影响。在非反应平面燃烧室试验段的中间平面上进行了二维双分量PIV测量。为支持实验观测,对选定的情况进行了三维数值模拟。在先前的一项研究中,在相同的设置中,研究了没有耀斑扩展的反向旋转径向旋流器。在本研究中,除了先前研究的基线旋流器几何形状外,还研究了四种不同的旋流器,它们具有三种不同的耀斑几何形状(一个半径为4毫米的圆形耀斑几何形状和两个角为27.5°和45°的倒角耀斑),圆形耀斑具有同向和反向旋转配置。时间平均流场分析表明,由于耀斑几何形状的引入,径向速度值增加,轴向速度值减少,导致旋涡射流的突然膨胀。当比较不同的耀斑几何形状时,可以观察到几乎相同的流场,并且对于使用耀斑几何形状的任何几何形状都没有观察到CRZ的形成。虽然几何形状的最大负轴向速度值减小,但由于再循环半径的增加,再循环质量流量高于基线涡旋器。另一方面,由于沿射流中心轴的逆压梯度更大,与逆旋转结构相比,同向旋转结构的再循环质量流量更高。采用快照POD方法识别了相干流结构,并报道了具有和不具有耀斑几何形状的旋流器的不同模态振型。结果表明,在给定旋流数和约束条件下,旋转感和耀斑几何形状的变化不会引起POD模态及其能量含量的变化。
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