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A method of predicting flow rates required to achieve anti-icing performance with a porous leading edge ice protection system

机译:一种利用多孔前缘防冰系统预测实现防冰性能所需的流速的方法

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摘要

A proposed method of analytically predicting the minimum fluid flow rate required to provide anti-ice protection with a porous leading edge system on a wing under a given set of flight conditions is presented. Results of the proposed method are compared with the actual results of an icing test of a real wing section in the NASA Lewis Icing Research Tunnel.

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