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Gas-Turbine Engine Air enters the compressor of a gas-turbine engine at 100kPa and 25C. The engine is designed with a pressure ratio of 5 .
Gas-Turbine Engine Air enters the compressor of a gas-turbine engine at 100kPa and 25C. The engine is designed with a pressure ratio of 5 . The maximum temperature in the engine is 850 C. A) What is the temperature of the air at the outlet of the compressor? B) What is the specific work produced in the compressor? C) What is the temperature of the air at the outlet of the turbine? D) What is the specific work produced in the turbine? A)200K364K412K472KB)175kJ/kg182kJ/kg196kJ/kg205kJ/kgC)436K589K709K1,123KD)389kJ/kg416kJ/kg427kJ/kg435kJ/kg
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