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Numerical Study of Momentum and Heat Transfer in Propylene Glycol Jets used for Aircraft Ground Deicing

机译:飞机地面除冰用丙二醇射流动量和传热的数值研究。

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Liquid jets are widely used in cleaning operations in the ground deicing aircraft sector. The present work investigates heat transfer and momentum forces created by hot turbulent propylene glycol jet impinging on a horizontal plate at temperature below zero point A cylindrical liquid jet impinging on an horizontal plate flows radially outwards from the point of impingement to form a wall film. A model for the simulation of aircraft ground de-icing is proposed. It is conjectured that flow due to impinging hot oblique jet on a horizontal plate depend mostly on the nozzle diameter, the jet velocity, the nozzle pressure, the jet inclination angle and the distance to plate (standoff). The Volume Of Fluid (VOF) model coupled with the film formulation is employed using Computational Fluid Dynamics (CFD) to capture the interface in multiphase flow (propylene glycol-ice-air). The three-dimensional Navier-Stokes and energy equations are numerically solved using a finite-volume discretization under steady and unsteady conditions with the RANS turbulence models. A conjugate heat transfer formulation is used to couple the heat transfer at the interface between the solid and fluid. Comparisons are made between CFD results and experimental observations reported in the literature for heat transfer prediction, and a good agreement between these two can be observed. This work is novel in that it first proposes a model to study parameters that govern deicing with propylene glycol jet.
机译:液体喷射器广泛用于地面除冰飞机领域的清洁操作。本工作研究了热的湍流丙二醇射流在低于零点的温度下撞击水平板上时产生的传热和动量力。撞击在水平板上的圆柱形液体射流从撞击点径向向外流动,从而形成壁膜。提出了一种飞机地面除冰仿真模型。据推测,由于将热倾斜射流撞击在水平板上而引起的流动主要取决于喷嘴直径,射流速度,喷嘴压力,射流倾斜角和到板的距离(对峙)。使用计算流体动力学(CFD),将流体体积(VOF)模型与薄膜配方结合使用,以捕获多相流(丙二醇-冰-空气)中的界面。使用RANS湍流模型,在稳态和非稳态条件下,使用有限体积离散化方法对三维Navier-Stokes和能量方程进行数值求解。共轭传热制剂用于在固体和流体之间的界面处耦合传热。比较了CFD结果和文献中报道的用于传热预测的实验观察结果,并且可以观察到两者之间的良好一致性。这项工作是新颖的,因为它首先提出了一个模型来研究用丙二醇射流控制除冰的参数。

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