Turbine blade of alloy steel (k = 29 W/mK, 6 cm long, Acs = 500'2mm and
p=12 cm) is exposed to hot gases of 820'C. The root temperature is 480°C. Determine
the temperature in the middle of the blade and heat loss from the blade. Takeh=320
W/m2K
(GTU Exam)
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