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首页> 外文期刊>Journal of Thermal Spray Technology >Numerical Modeling of Suspension HVOF Spray
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Numerical Modeling of Suspension HVOF Spray

机译:悬浮HVOF喷雾的数值模拟

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A three-dimensional two-way coupled Eulerian-Lagrangian scheme is used to simulate suspension high-velocity oxy-fuel spraying process. The mass, momentum, energy, and species equations are solved together with the realizable k-epsilon turbulence model to simulate the gas phase. Suspension is assumed to be a mixture of solid particles [mullite powder (3Al(2)O(3)center dot 2SiO(2))], ethanol, and ethylene glycol. The process involves premixed combustion of oxygen-propylene, and non-premixed combustion of oxygen-ethanol and oxygen-ethylene glycol. One-step global reaction is used for each mentioned reaction together with eddy dissipation model to compute the reaction rate. To simulate the droplet breakup, Taylor Analogy Breakup model is applied. After the completion of droplet breakup, and solvent evaporation/ combustion, the solid suspended particles are tracked through the domain to determine the characteristics of the coating particles. Numerical simulations are validated against the experimental results in the literature for the same operating conditions. Seven or possibly eight shock diamonds are captured outside the nozzle. In addition, a good agreement between the predicted particle temperature, velocity, and diameter, and the experiment is obtained. It is shown that as the standoff distance increases, the particle temperature and velocity reduce. Furthermore, a correlation is proposed to determine the spray cross-sectional diameter and estimate the particle trajectories as a function of standoff distance.
机译:采用三维双向耦合的欧拉-拉格朗日方案模拟悬浮液高速含氧燃料的喷射过程。将质量,动量,能量和物质方程式与可实现的k-ε湍流模型一起求解,以模拟气相。悬浮液假定为固体颗粒[莫来石粉(3Al(2)O(3)中心点2SiO(2))],乙醇和乙二醇的混合物。该方法涉及氧-丙烯的预混合燃烧,以及氧-乙醇和氧-乙二醇的非预混合燃烧。对于提到的每个反应,均采用一步全局反应以及涡流耗散模型来计算反应速率。为了模拟液滴破裂,应用泰勒类比破裂模型。液滴破裂完成,溶剂蒸发/燃烧完成后,通过该区域跟踪固体悬浮颗粒,以确定涂层颗粒的特性。对于相同的工作条件,数值模拟已针对文献中的实验结果进行了验证。喷嘴外面捕获了七个或八个冲击钻石。此外,在预测的粒子温度,速度和直径与实验之间也取得了良好的一致性。结果表明,随着间隔距离的增加,颗粒温度和速度降低。此外,提出了一种相关性,用于确定喷雾横截面直径和估计粒子轨迹,作为支座距离的函数。

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