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Effect of flow confinement on the hydrodynamics and heat transfer characteristics of swirling impinging jets

机译:流动限制对旋转冲击喷射的流体动力学和传热特性的影响

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Although confined swirling jets are typically used in many practical applications, a detailed investigation in the literature is, however, very limited. As such, this paper investigates the fundamental thermofluidic behaviors of swirling impinging jets due to flow confinements at small impingement distance. In this regard, turbulent flow simulations with an ambient air jet are carried out using RANS approach, whereby turbulence is governed by SST k-ω model. Inlet boundary conditions are applied from the CTA anemometer derived experimental data for the same nozzle geometry in order for a realistic analysis. The flow dynamics and heat transfer between a swirling jet and the impingement plate are studied for a Reynolds number (Re) equals to 11,600 and Swirl numbers (S) from 0 to 0.74 for an impingement distance equals to 0.5 nozzle diameter. The results show that a strong flow recirculation zone appears between the nozzle and the surface, even for non-swirling jets. For highly swirling jets, another secondary recirculation zone exists around the central axis near the stagnation point. The surface static pressure distribution is found to be negative due to flow confinement for all swirl conditions. The degree of swirl intensity and the associated flow recirculation also largely affect heat transfer behaviors on the impingement surface.
机译:虽然狭窄的旋转喷气机通常用于许多实际应用中,但是,文献中的详细调查是非常有限的。因此,本文研究了由于小冲击距离的流动限制而旋转撞击喷射的基本热流体行为。在这方面,使用RAN方法进行具有环境空气射流的湍流模拟,由此湍流由SST k-ω模型控制。入口边界条件从CTA风速计衍生的实验数据应用于相同的喷嘴几何形状,以便进行实际分析。研究旋转射流和冲击板之间的流动动力学和传热,用于雷诺数(RE)等于11,600,涡流距离的涡流数为0至0.74,撞击距离等于0.5喷嘴直径。结果表明,即使对于非旋流喷射,喷嘴和表面之间出现强流量再循环区域。对于高旋转的喷射,另一个次要再循环区域周围存在于滞留点附近的中心轴周围。由于所有涡流条件的流动限制,发现表面静压分布是负的。涡流和相关的流动再循环的程度在很大程度上影响冲击表面上的传热行为。

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