Water at 0°C releases 333.7 kJ/kg of heat as it freezes to ice (ρ = 920 kg/m3) at 0°C. An aircraft flying under icing conditions maintains a heat transfer coefficient of 150 W/m2∙K between the air and wing surfaces. What temperature must the wings be maintained at to prevent ice from forming on them during icing conditions at a rate of 1 mm/min or less?
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