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Inflow characteristics for generating axis-switching phenomenon of heated rectangular jets

机译:加热矩形喷射轴切换现象的流入特性

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Flow characteristics due to the axis-switching phenomenon are numerically investigated for heated rectangular jets with typical inlet conditions and three aspect ratios (AR), namely 1.0, 1.5, and 2.0. To examine various inlets and their relation to the axis-switching flow, an inflow generator is newly devised, wherein jet flows from an orifice plate and a long pipe nozzle can be realized. Depending on the inlet conditions, the 45. and 90 degrees axis-switching phenomena for the rectangular jet are observed to appear differently. As the aspect ratio increases and jet temperature decreases, the axis-switching positions are delayed downstream. It is observed that the strong and weak states of the axis-switching flows can be interpreted by the crossover locations of the jet half-widths and the saddle-shaped velocity profile is not the only main factor for axis-switching flow. As the jet temperature increases, a well-mixed state is quickly obtained, and the mixing performance of the square jet is better than that of the rectangular jet. For both isothermal and heated jets, the flow mixing is improved by the axis-switching flow. Various analyses are attempted to find the specific inlet structure for the axis-switching flow. From the results, the special features for inflow criterion producing axis-switching flow can be explained by factors such as the deformation parameter, interrelations between shear strain and normal rates, turbulence-driven and geometry-driven streamwise vortices, and normal Reynolds stresses.
机译:对于具有典型入口条件的加热矩形喷射和三个纵横比(AR),即1.0,1.5和2.0,对由于轴切换现象引起的流动特性进行了数值研究。为了检查各种入口及其与轴切换流的关系,新设计流入发生器,其中可以实现从孔板和长管喷嘴的喷射流动。根据入口条件,观察到矩形射流的45和90度轴切换现象以不同地出现。随着纵横比增加和喷射温度降低,轴切换位置被延迟下游。观察到,轴切换流的强度和弱状态可以通过射流半宽的交叉位置来解释,并且鞍形速度曲线不是轴切换流的唯一主因子。随着喷射温度的增加,快速获得良好的混合状态,方形射流的混合性能优于矩形射流的混合性能。对于两种等温和加热的喷射,通过轴切换流改善流动混合。尝试各种分析来找到轴切换流的特定入口结构。从结果,可以通过诸如变形参数,剪切应变和正常速率之间的相互关系,湍流驱动和几何驱动的流动涡流的因素来解释产生轴切换流的特殊功能,可以解释诸如变形参数,湍流驱动和几何形状的流动涡流,以及正常的雷诺应力。

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