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Consider the gas turbine cooling scheme of Example 43 In Problem 323 advantages associated with applying a thermal barrier coating TBC to the exterior surface of a turbine blade are described

Consider the gas turbine cooling scheme of Example 4.3. In Problem 3.23, advantages associated with applying a thermal barrier coating (TBC) to the exterior surface of a turbine blade are described. If a 0.5-mm-thick zirconia coating (k = 1.3 W/m∙ K,  is applied to the outer surface of the air-cooled blade, determine the temperature field in the blade for the operating conditions of Example 4.3.

 

Jun 27 2020 View more View Less

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