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In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.? for Mechanical Engineering 2024 is part of Mechanical Engineering preparation. The Question and answers have been prepared according to the Mechanical Engineering exam syllabus. Information about In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.? covers all topics & solutions for Mechanical Engineering 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.?.

Solutions for In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.? in English & in Hindi are available as part of our courses for Mechanical Engineering. Download more important topics, notes, lectures and mock test series for Mechanical Engineering Exam by signing up for free.

Here you can find the meaning of In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.? defined & explained in the simplest way possible. Besides giving the explanation of In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.?, a detailed solution for In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.? has been provided alongside types of In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.? theory, EduRev gives you an ample number of questions to practice In a gas turbine the gas enters at the rate of 5 Kg/s with a velocity of 50m/s and enthalpy of 900KJ/kg and leaves the turbine with a velocity of 150 m/s and enthalpy of 400 KJ/kg. The loss of heat from the gas to the surroundings is 25 KJ/kg. Assume for gas R = 287 KJ/kg K and Cp 1.004 KJ/kg K and the inlet conditions to be at 100KPa and 27oC. Determine the power output of the turbine and the diameter of the inlet pipe.? tests, examples and also practice Mechanical Engineering tests.