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  • 1
    Publication Date: 2019-06-28
    Description: Several methods of cyclic de-icing of a gas-heated airfoil were investigated to determine ice-removal characteristics and heating requirements. The cyclic de-icing system with a spanwise ice-free parting strip in the stagnation region and a constant-temperature gas-supply duct gave the quickest and most reliable ice removal. Heating requirements for the several methods of cyclic de-icing are compared, and the savings over continuous ice prevention are shown. Data are presented to show the relation of surface temperature, rate of surface heating, and heating time to the removal of ice.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NACA-RM-E53C27
    Format: application/pdf
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