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2. A turbine blade in a gas turbine jet engine is shown. The turbine blade has a thermal barrier coating (TBC) made of a Zirconia ceramic applied to the exterior blade which is made of a high temperature superalloy Inconel. Cooling air flows internal to the blade, and convection also occurs on the exterior of the blade. 1000 W2 1700 K 400 K Incone Assuming that the turbine blade can be modeled as a plane wall as shown, find; a) Draw the equivalent electrical circuit for heat flow across the turbine blade. b) Find the total thermal resistance across the turbine blade if a contact resistance of R-1 x 10m2 K/W exists between the Zirconia ceramic and the Inconel. Hint: Work on a per unit area basis, e.g. cross sectional area of the plane w(turbine blade) will not appear in any of the resistance terms. c) Find the heat flux q across the turbine blade d) Find the maximum temperature in the Inconel.
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