A turbine blade, 6.25 cm long, cross-sectional area 4.5 cm2, perimeter 12 cm, is made of stainless steel (k = 26.16 W/m K). The temperature of the root is 500°C. The blade is exposed to a hot gas at 800°C, and the average heat transfer coefficient is 0.465 kW/m2K. Determine the temperature and the rate of heat flow at the root of the blade. Assume that the tip is insulated.
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