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The Pressure ratio across a gas turbine (for air, specific heat at constant pressure, pc = 1040J / kg. K and ratio of specific heats, γ = 1.4) is 10. If the inlet temperature to the turbine is 1200K and the isentropic efficiency is 0.9, the gas temperature at turbine exit is ______ K.Correct answer is between '675,684'. Can you explain this answer? for GATE 2024 is part of GATE preparation. The Question and answers have been prepared according to the GATE exam syllabus. Information about The Pressure ratio across a gas turbine (for air, specific heat at constant pressure, pc = 1040J / kg. K and ratio of specific heats, γ = 1.4) is 10. If the inlet temperature to the turbine is 1200K and the isentropic efficiency is 0.9, the gas temperature at turbine exit is ______ K.Correct answer is between '675,684'. Can you explain this answer? covers all topics & solutions for GATE 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for The Pressure ratio across a gas turbine (for air, specific heat at constant pressure, pc = 1040J / kg. K and ratio of specific heats, γ = 1.4) is 10. If the inlet temperature to the turbine is 1200K and the isentropic efficiency is 0.9, the gas temperature at turbine exit is ______ K.Correct answer is between '675,684'. Can you explain this answer?.

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