Question 2) A gas-turbine power plant operates on a gas-turbine cycle which has the pressure ratio of 6. At the compressor inlet and turbine inlet, the gas temperature values are 400 K and 1550 K, respectively. The compressor efficiency is 78% and the turbine efficiency is 87%. Considering, the air-standard assumptions, a) determine the isentropic exit temperature values of the compressor and turbine components, b) determine the real exit temperature values of the compressor and turbine components, c) Find the thermal efficiency of the gas-turbine

Question 2) A gas-turbine power plant operates on a gas-turbine cycle which has the pressure ratio of 6. At the compressor inlet and turbine inlet, the gas temperature values are 400 K and 1550 K, respectively. The compressor efficiency is 78% and the turbine efficiency is 87%. Considering, the air-standard assumptions, a) determine the isentropic exit temperature values of the compressor and turbine components, b) determine the real exit temperature values of the compressor and turbine components, c) Find the thermal efficiency of the gas-turbine

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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T5.1
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