A gas turbine power plant operating on a Brayton cycle takes in atmospheric air at 16°C. The temperature of the air rises by 218°C over the compressor, and by a further 729°C over the combustion chamber. If the heating value of the fuel burned in the turbine is 40 MJ/kg, calculate the rate in kg/s at which fuel must be burned for each MW of output from the power plant. Give your answer to three decimal places. Take the specific heat capacity c, of air to be 1.005 kJ/(kg K), and the ratio of specific heats k to be 1.4. You may also assume that changes in the properties of the air due to the addition and combustion of fuel are negligible.

A gas turbine power plant operating on a Brayton cycle takes in atmospheric air at 16°C. The temperature of the air rises by 218°C over the compressor, and by a further 729°C over the combustion chamber. If the heating value of the fuel burned in the turbine is 40 MJ/kg, calculate the rate in kg/s at which fuel must be burned for each MW of output from the power plant. Give your answer to three decimal places. Take the specific heat capacity c, of air to be 1.005 kJ/(kg K), and the ratio of specific heats k to be 1.4. You may also assume that changes in the properties of the air due to the addition and combustion of fuel are negligible.

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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