Consider an ideal gas-turbine cycle with a pressure ratio across the compressor of 12:1. The compressor inlet is at 300 K, 100 kPa, and the cycle has a maximum temperature of 1327 oC with a regenerator having an effectiveness of 80%. Find (a) the air temperature entering the combustor and (b) the thermal efficiency of the cycle. Use cold air properties at room temperature (cp = 1.00 kJ/kg-K, k = 1.4). 61-80. Consider an ideal gas-turbine cycle with a pressure ratio across the compressor of 12:1.The compressor inlet is at 300 K, 100 kPa, and the cycle has a maximum temperature of 1327°C with a regenerator having an effectiveness of 80%. Find (a) the air temperature entering thecombustor and (b) the thermal efficiency of the cycle. Use cold air properties at roomtemperature (c, = 1.00 kJ/kg-K, k = 1.4).%3D

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Answered: 61-80. Consider an ideal gas-turbine…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

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Consider an ideal gas-turbine cycle with a pressure ratio across the compressor of 12:1. The compressor inlet is at 300 K, 100 kPa, and the cycle has a maximum temperature of 1327 oC with a regenerator having an effectiveness of 80%. Find (a) the air temperature entering the combustor and (b) the thermal efficiency of the cycle. Use cold air properties at room temperature (cp = 1.00 kJ/kg-K, k = 1.4).

61-80. Consider an ideal gas-turbine cycle with a pressure ratio across the compressor of 12:1.
The compressor inlet is at 300 K, 100 kPa, and the cycle has a maximum temperature of 1327
°C with a regenerator having an effectiveness of 80%. Find (a) the air temperature entering the
combustor and (b) the thermal efficiency of the cycle. Use cold air properties at room
temperature (c, = 1.00 kJ/kg-K, k = 1.4).
%3D

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