首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >EXPERIMENTAL VALIDATION OF METHODS PROVIDING BOUNDARY CONDITIONS TO SIMULATE THE EVAPORATION PROCESS OF WATER INJECTED INTO HIGH SPEED AIR FLOW
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EXPERIMENTAL VALIDATION OF METHODS PROVIDING BOUNDARY CONDITIONS TO SIMULATE THE EVAPORATION PROCESS OF WATER INJECTED INTO HIGH SPEED AIR FLOW

机译:提供边界条件以模拟注入高速气流中水蒸发过程的方法的实验验证

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Water injection into a high speed air flow has been recently investigated by many scientists and is still an important field of research in gas turbine technology. To study the behavior of droplets in gas turbines, expensive experimental tests and their validation with analytical and Computational Fluid Dynamics (CFD) models are necessary. The Euler-Lagrange approach can be used to tackle these problems due to their capability in tracking particles along the domain, relative ease in formulating and applying them to the current industrial problems in terms of acceptable computational cost. However, providing spray boundary conditions using Euler-Lagrange approach is quite challenging because the spray pattern depends upon various parameters like spray angle, velocity, diameter distribution etc. In this paper, to obtain these parameters, two different approaches are described. The first approach depends on an analytical model for velocity and spray angle injection conditions and the second approach depends on an Euler free surface simulation. For diameter distribution, Rosin Rammler distribution function and experimental data are used. When combined together these lead to four particle injection conditions. The results achieved from all the four cases are compared with the experimental data of water droplet evaporation in a high speed air flow obtained from a hot air test rig operating at conditions of real gas turbines.
机译:最近,许多科学家已经研究了向高速气流中注水的问题,这仍然是燃气轮机技术研究的重要领域。为了研究燃气轮机中的液滴行为,必须进行昂贵的实验测试并通过分析和计算流体动力学(CFD)模型对其进行验证。 Euler-Lagrange方法可以解决这些问题,这是因为它们具有沿区域跟踪粒子的能力,并且在可接受的计算成本方面相对容易制定和将其应用于当前的工业问题。然而,使用欧拉-拉格朗日方法提供喷雾边界条件非常具有挑战性,因为喷雾模式取决于各种参数,例如喷雾角度,速度,直径分布等。在本文中,为获得这些参数,描述了两种不同的方法。第一种方法取决于速度和喷雾角度喷射条件的分析模型,第二种方法取决于Euler自由表面模拟。对于直径分布,使用松香拉姆勒分布函数和实验数据。当组合在一起时,将导致四个粒子注入条件。将这四种情况获得的结果与从在真实燃气轮机条件下运行的热空气试验台获得的高速气流中水滴蒸发的实验数据进行比较。

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