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MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM

机译:声学治疗的机舱唇源型抗糖浆系统的建模

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Acoustically treated nacelle lip transpiration flow anti-icing system is analyzed by solving the two dimensional transient heat conduction equation with a combined transpiration flow convective heat transfer and thermodynamics energy transfer rate boundary condition. The nacelle lip skin surface temperature distribution is determined when the skin exposed to airflow laden with atmospheric cloud super cooled water droplets of known size distribution is heated using transpiration air flow.
机译:通过求解具有组合蒸腾流动对流传热和热力学能量传递速率边界条件的二维瞬态导热方程来分析声学处理的机舱唇液蒸腾流动抗糖浆系统。当通过蒸腾空气流动加热暴露于带有大气云超冷却水滴的气体暴露于空气流量的皮肤的皮肤时,确定机舱唇形表面温度分布。

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