Air enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 ⁰C with a low velocity and exits at 1 MPa and 347 ⁰C with a velocity of 90 m/s. The compression process is reversible adiabatic, and the power input is 265 W. Determine the mass flowrate of the air through the compressor. Solve this problem using property table.

Q: Air enters a compressor at ambient conditions of 100 kPa and 20°C at a rate of 6.2 m3 /s with a low…

A: Given Inlet conditions Pressure =100 kPa Temperature = 20o C Mass flow rate = 6.2 m3/s Outlet…

Q: An adiabatic air compressor is to be powered by a direct-coupled adiabatic steam turbine that is…

A: Given Data:

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Q: Air enters the compressor of a gas-turbine plant at ambient conditions of 100 kPa and 25°C with a…

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Q: Steam enters an adiabatic turbine at 10 MPa and 400°C with a mass flow rate of 4.5 kg/s and leaves…

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Q: Steam enters an adiabatic turbine at 2Mpa and 250C and expands to 25kPa with an isentropic…

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Q: Refrigerant-134a at 140 kPa and –10°C is compressed by an adiabatic 1.3-kW compressor to an exit…

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Q: Q3: Steam enters an adiabatic turbine at 8 MPa, 550°C, and 15 m/s and leaves at 60 kPa, 150°C, and…

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Q: Air enters an adiabatic nozzle steadily at 300 Kpa, 200 °C and 30 m's then leaves at 100 Kpa and 180…

A:

Q: Air enters a compressor at ambient conditions of 100 kPa and 20°C at a rate of 6.2 m3 /s with a low…

A: Mass flow rate for air can be determined by using ideal gas equation Work done on compressor in…

Q: Air enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 ⁰C with a…

A: Given:-Air enter at 100 kPa, 25°C, low velocity, V1Air exit at 1 MPa,  347 ⁰CQadabatic=0Power…

Q: Air enters the compressor of a gas-turbine plant at ambient conditions of 100 kPa and 25°C with a…

A: Given data: Inlet temperature of air, T1 = 250C = 298 K Exit temperature of air, T2 = 3470C = 620 K…

Q: Air enters the compressor of a gas-turbine plant at ambient conditions of 100 kPa and 25 °C with a…

A:

Q: Steam enters an adiabatic turbine at 5 MPa, 650C, and 80 m/s and leaves at 50 kPa, 1508C, and 140…

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Q: Air enters the compressor of a gas-turbine plant at ambient conditions of 100 kPa and 25°C with a…

A:

Q: Steam enters an adiabatic turbine steadily at 7 MPa, 500°C, and 45 m/s and leaves at 100 kPa and 75…

A: Write the given data:

Q: Steam enters an adiabatic turbine at 5 MPa, 650 °C, and 80 m/s and leaves at 50 kPa, 150 °C, and 140…

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Q: ater flows through a horizontal coil heated from the outside by high temperature flue gases. As it…

A: given

Q: Steam enters an adiabatic nozzle at 2 MPa and 350°C with a velocity of 55 m/s and exits at 0.8 MPa…

A: First, need to find the actual enthalpy…

Q: Air enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 ⁰C with a…

A:

Q: Two rigid tanks are connected by a valve. Tank A is insulated and contains 0.3 m3 of steam at 400…

A: Given data Pressure in rigid tank A is: PA=400 kPa. The quality of steam in tank A is: x=60%. The…

Q: Air is compressed in a car engine from 22°C and 95 kPa in a reversible and adiabatic manner. If the…

A:

Q: Air enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 ⁰C with a…

A: ANSWER MASS FLOWRATE 0.808 Kg/s   Solution is given below.

Q: Air enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 ⁰C with a…

A:

Q: Air is compressed by an adiabatic compressor from 95 kPa and 27°C to 600 kPa and 277°C. Assuming…

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Q: Air enters the compressor of a gas-turbine plant at ambient conditions of 100 kPa and 25°C with a…

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Q: Steam flows steadily through an adiabatic turbine. The inlet conditions of the steam are 10 MPa, 450…

A: The change in the kinetic energy can be determined as,

Q: Steam enters an adiabatic turbine at 5 MPa and 500°C with a 50 m/s velocity and exits from the…

A: Question (a) and (b) are solved here. For question (c), please post this question again.

Q: Air is compressed isothermally from 13 psia and 55°F to 80 psia in a reversible steady-flow device.…

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Q: Q5 (a) Air enters an adiabatic compressor at 100 kPa and 17°C at a rate of 2.4 m³/s, and it exits at…

A:

Q: Air enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 °C with a…

A:

Q: Air enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 ⁰C with a…

A:

Q: Air enters the compressor of a gas turbine plant at ambient conditions of 100 kPa and 25 ⁰C with a…

A:

Q: Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180…

A:

Q: (a) Air enters an adiabatic compressor at 100 kPa and 17°C at a rate of 2.4 m³/s, and it exits at…

A: Given data :- P1 =100kpa T1=17°C T2=270°C Flow rate =2.4 m^3/sec

Q: Refrigerant R-134a at 500 kPa and 191 enters an adiabatic nozzle steadily with a velocity of 15 cm/s…

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Q: Refrigerant-134a at 140 kPa and –10°C is compressed by an adiabatic 1.3-kW compressor to an exit…

A: find out the final enthalpy by using R134a table…

Q: Water at 20 psia and 500F enters a mixing chamber at a rate of 7 lbm/s where it is mixed steadily…

A:

Q: Air enters an adiabatic chamber steadily at 300kPa, 200 C, and 45 m/s. It leaves at 100 kPa and 180…

A: The total energy material of a control volume stays unchanged during a steady process flow. i.e.,…