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Uniform Design Correlations for Glaze Ice Accretion and Convective Heat Transfer from an Airfoil

机译:翼型釉冰积聚和对流传热的统一设计相关性

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Heat transfer with ice accretion are encountered in a range of problems such as icing of aircraft, wind turbine blades, overhead power transmission lines, and others. Northern and offshore locations have promising wind potential, however, challenges with icing occur when the turbine is exposed to sea-spray and precipitation at sub-zero temperatures. The droplets impact and freeze on blade surfaces causing significant reduction in power output and turbine longevity, as well as creating safety hazards from ice shedding. Ice accretion modelling for aircraft, wind turbines, and power transmission cables has led to the development of computational fluid dynamics (CFD) ice simulation packages, such as LEWICE and FENSAP-ICE. These can be used to relate ice accretion on a specified geometry exposed to different climatic conditions, including liquid water content, droplet diameters, relative air speed, and air temperature. Ice accretion responses that can be analyzed include changes in geometry, aerodynamic changes, ice growth rates, and heat fluxes. In this paper, a uniform experimental design approach is applied to numerical predictions to develop new ice accretion correlations over a range of climatic conditions. The results are correlated into closed-form estimates for relevant ice accretion factors in terms of the Nusselt number and ice thickness. A new rime glaze ice transition parameter R* is proposed and validated to predict how climatic conditions influence whether rime or glaze ice formation will occur on an airfoil surface.
机译:积冰的传热在一系列问题中遇到,例如飞机结冰,风力涡轮机叶片,架空输电线等。北部和近海地区的风能潜力很大,但是,当涡轮机暴露于零下温度下的海浪和降雨中时,会出现结冰的挑战。水滴撞击并冻结在叶片表面上,从而导致功率输出和涡轮寿命的显着降低,并因冰块脱落而造成安全隐患。用于飞机,风力涡轮机和输电电缆的积冰模型导致了计算流体动力学(CFD)冰仿真程序包的开发,例如LEWICE和FENSAP-ICE。这些可用于将冰的积聚与暴露于不同气候条件(包括液态水含量,液滴直径,相对空气速度和空气温度)的指定几何形状相关。可以分析的积冰响应包括几何形状变化,空气动力学变化,冰生长速率和热通量。在本文中,将统一的实验设计方法应用于数值预测,以在一定的气候条件下开发新的积冰关系。将结果关联到有关努氏数和冰厚度的相关冰积因子的封闭式估计中。提出并验证了新的霜冰釉过渡参数R *,以预测气候条件如何影响翼型表面上的霜或釉冰形成。

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