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airfoil were investigated Airspeed angle of attack Bowden characteristics and heating continuous anti-icing cubic meter cycle ratio cyclic de-icing system datum air temperature determine ice-removal characteristics Distance from zero dry-air foot span gas flow gas-heated airfoil gas-supply duct gave gave the quickest gram per cubic Gray and Dean heat flow heat of fusion heat-off heat-on period heat-source requirement heating period hour per foot Ice shed ice-free parting strip ice-shedding icing conditions icing period increase leading edge liquid-water content marginal de-icing methods of cyclic miles per hour NACA RM E53C27 plenum chamber pounds per hour Prevention and Removal prevention are shown rate of surface rear passage reliable ice removal Removal 7.3 RM E53C27 National runback icing savings over continuous shown in figure slip joint spanwise ice-free stagnation point stagnation region supply duct surface heating surface temperature temperature gas-supply duct thermocouples Total air temperature upper surface Vernon H zero chord