Conduction1. A thermodynamic analysis of a proposed Brayton cycle gas turbine yields P=5 MW of net power production. The compressor, at an average temperatureof T. = 400°C, is driven by the turbine at an average temperature of T₁ =1000°C by way of an L = 1m-long, d= 70mm - diameter shaft of thermalconductivity k = 40 W/m K.CompressorminTCombustionchamberShaftLTurbineThout(a) Compare the steady-state conduction rate through the shaft connecting the hotturbine to the warm compressor to the net power predicted by the thermodynamics-based analysis.(b) A research team proposes to scale down the gas turbine of part (a), keeping alldimensions in the same proportions. The team assumes that the same hot and coldtemperatures exist as in part (a) and that the net power output of the gas turbine isproportional to the overall volume of the device. Plot the ratio of the conduction throughthe shaft to the net power output of the turbine over the range 0.005 m s Ls 1 m. Is ascaled-down device with L = 0.005 m feasible?

Given-Information:- Net power, P = 5 MWCompressor Temperature, Tc =400°Cdriven,Th = 1000°CLength, L…

Conduction 1. A thermodynamic analysis of a proposed Brayton cycle gas turbine yie 5 MW of net power production. The compressor, at an average temper of T = 400°C, is driven by the turbine at an average temperature of Th 1000°C by way of an L = 1m-long, d= 70mm - diameter shaft of therm conductivity k = 40 W/m K. Compressor Combustion chamber Turbine d

Conduction 1. A thermodynamic analysis of a proposed Brayton cycle gas turbine yie 5 MW of net power production. The compressor, at an average temper of T = 400°C, is driven by the turbine at an average temperature of Th 1000°C by way of an L = 1m-long, d= 70mm - diameter shaft of therm conductivity k = 40 W/m K. Compressor Combustion chamber Turbine d

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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