Question: Problem 3 ( 1 0 points ) - Second law analysis of nozzles Hot combustion gases enter the nozzle of a gas turbine at 3

Problem 3(10 points)- Second law analysis of nozzles
Hot combustion gases enter the nozzle of a gas turbine at 320 kPa and \(747^{\circ}\mathrm{C}\) and \(100\mathrm{~m}/\mathrm{s}\) and exit to a pressure of 90 kPa . You are working on the selection of the nozzle that will deliver a minimum exit temperature of \(525^{\circ}\mathrm{C}\). For this application, you are considering a nozzle with isentropic efficiency rated at \(92\%\). In your analysis you decide to use the method of variable specific heats along with other assumptions that you will list. Will this nozzle satisfy your operation requirements?
Problem 3 ( 1 0 points ) - Second law analysis of

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