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16 October, 04:36

A turbine blade made of a metal alloy (k = 17 W/m-K) has a length of 5.3 cm, a perimeter of 11 cm, and a cross-sectionalarea of 513 cm2 The turbine blade is exposed to hot gas from the combustion Chamber at 973°C with a convection heattransfer coefficient of 538 W/mZ-K The base of the turbine blade maintains a constant temperature of 450°C and the tip isadiabatic. Determine the heat transfer rate to the turbine blade and temperature at the tip-

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  1. 16 October, 06:12
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    hey sherlock!

    Explanation:

    figure it out on ur own!
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