Deck 5: Mass and Energy Analysis of Control Volumes
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Deck 5: Mass and Energy Analysis of Control Volumes
1
Steam is accelerated by a nozzle steadily from a low velocity to a velocity of 220 m/s at a rate of 1.2 kg/s. If the steam at the nozzle exit is at 300°C and 2 MPa, the exit area of the nozzle is
A)6.8 cm2
B)7.2 cm2
C)3.8 cm2
D)54.6 cm2
E)22.8 cm2
A)6.8 cm2
B)7.2 cm2
C)3.8 cm2
D)54.6 cm2
E)22.8 cm2
6.8 cm2
2
Refrigerant 134a enters a diffuser steadily at 0.5 MPa, 50°C, and 120 m/s at a rate of 1.2 kg/s. The inlet area of the diffuser is
A)0.81 cm2
B)4.8 cm2
C)26 cm2
D)5.3 cm2
E)100 cm2
A)0.81 cm2
B)4.8 cm2
C)26 cm2
D)5.3 cm2
E)100 cm2
4.8 cm2
3
An adiabatic heat exchanger is used to heat cold water at 8°C entering at a rate of 3 kg/s by hot air at 150°C entering also at rate of 3 kg/s. If the exit temperature of hot air is 30°C, the exit temperature of cold water is (use constant specific heats at room temperature)
A)150°C
B)30°C
C)36.9°C
D)28.6°C
E)128°C
A)150°C
B)30°C
C)36.9°C
D)28.6°C
E)128°C
36.9°C
4
A heat exchanger is used to heat cold water at 8°C entering at a rate of 1.2 kg/s by hot air at 90°C entering at rate of 2.5 kg/s. The heat exchanger is not insulated, and is loosing heat at a rate of 28 kJ/s. If the exit temperature of hot air is 20°C, the exit temperature of cold water is (use constant specific heats at room temperature)
A)43.1°C
B)48.6°C
C)78.0°C
D)37.5°C
E)27.5°C
A)43.1°C
B)48.6°C
C)78.0°C
D)37.5°C
E)27.5°C
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5
An adiabatic heat exchanger is used to heat cold water at 12°C entering at a rate of 4 kg/s by hot water entering at 95°C at rate of 2.5 kg/s. If the exit temperature of hot water is 50°C, the exit temperature of cold water is
A)90°C
B)50°C
C)95°C
D)57°C
E)40°C
A)90°C
B)50°C
C)95°C
D)57°C
E)40°C
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6
In a water heating system, cold water at 5°C flowing at a rate of 5 kg/s is mixed adiabatically with hot water at 80°C flowing at a rate of 2 kg/s. The exit temperature of the mixture is
A)26.4°C
B)42.5°C
C)40.0°C
D)64.3°C
E)55.2°C
A)26.4°C
B)42.5°C
C)40.0°C
D)64.3°C
E)55.2°C
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7
In a heating system, cold outdoor air at 10°C flowing at a rate of 6 kg/min is mixed adiabatically with hot air at 50°C flowing at a rate of 1.5 kg/min. Assuming constant specific heats at room temperature, the exit temperature of the mixture is
A)30°C
B)18°C
C)45°C
D)22°C
E)38°C
A)30°C
B)18°C
C)45°C
D)22°C
E)38°C
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8
Hot combustion gases (assumed to have the properties of air at room temperature) enter a gas turbine at 0.8 MPa and 1500 K at a rate of 2.1 kg/s, and exit at 0.1 MPa and 800 K. If heat is lost from the turbine to the surroundings at a rate of 150 kJ/s, the power output of the gas turbine is
A)1477 kW
B)1677 kW
C)1327 kW
D)1124 kW
E)872 kW
A)1477 kW
B)1677 kW
C)1327 kW
D)1124 kW
E)872 kW
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9
Refrigerant-134a expands in an adiabatic turbine from 1 MPa and 120°C to 0.10 MPa and 50°C at a rate of 0.8 kg/s. The power output of the turbine is
A)72.5 kW
B)58.0 kW
C)43.5 kW
D)46.4 kW
E)54.4 kW
A)72.5 kW
B)58.0 kW
C)43.5 kW
D)46.4 kW
E)54.4 kW
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10
Steam expands in an adiabatic turbine from 4 MPa and 500°C to 0.5 MPa and 250°C at a rate of 1740 kg/h. The power output of the turbine is
A)1004 kW
B)485 kW
C)182 kW
D)377 kW
E)235 kW
A)1004 kW
B)485 kW
C)182 kW
D)377 kW
E)235 kW
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11
fSteam expands in a turbine from 6 MPa and 500°C to 0.2 MPa and 150°C at a rate of 1.2 kg/s. Heat is lost from the turbine at a rate of 34 kJ/s during the process. The power output of the turbine is
A)750 kW
B)784 kW
C)818 kW
D)573 kW
E)641 kW
A)750 kW
B)784 kW
C)818 kW
D)573 kW
E)641 kW
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12
Steam is compressed by an adiabatic compressor from 0.1 MPa and 100°C to 1.0 MPa and 400°C at a rate of 0.85 kg/s. The power input to the compressor is
A)692 kW
B)500 kW
C)383 kW
D)451 kW
E)588 kW
A)692 kW
B)500 kW
C)383 kW
D)451 kW
E)588 kW
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13
Refrigerant-134a is compressed by an adiabatic compressor from the saturated vapor state at 0.12 MPa to 1.2 MPa and 70°C at a rate of 0.108 kg/s. The power input to the compressor is
A)587 kW
B)63.4 kW
C)6.85 kW
D)6.42 kW
E)59.4 kW
A)587 kW
B)63.4 kW
C)6.85 kW
D)6.42 kW
E)59.4 kW
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14
Refrigerant-134a is compressed steadily from the saturated vapor state at 0.10 MPa to 1.4 MPa and 60°C at a rate of 0.15 kg/s. The refrigerant is cooled at a rate of 1.80 kJ/s during compression. The power input to the compressor is
A)5.74 kW
B)7.54 kW
C)9.08 kW
D)9.34 kW
E)46.7 kW
A)5.74 kW
B)7.54 kW
C)9.08 kW
D)9.34 kW
E)46.7 kW
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15
Saturated refrigerant 134a vapor at 40°C is condensed as it flows through a tube at a rate of 0.2 kg/s. The condensate leaves the tube as saturated liquid at 40°C. The rate of heat transfer from the tube is
A)21.0 kJ/s
B)53.4 kJ/s
C)162 kJ/s
D)74.4 kJ/s
E)32.4 kJ/s
A)21.0 kJ/s
B)53.4 kJ/s
C)162 kJ/s
D)74.4 kJ/s
E)32.4 kJ/s
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16
Helium gas is to be heated steadily by a 3-kW electric resistance heater as it flows through an insulated duct. If the helium enters at 50°C at a rate of 0.08 kg/s, the exit temperature of helium will be
A)57.2°C
B)50.6°C
C)62.0°C
D)71.9°C
E)112.0°C
A)57.2°C
B)50.6°C
C)62.0°C
D)71.9°C
E)112.0°C
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17
Air at 300 K and 200 kPa is throttled by a valve to a pressure of 100 kPa. If the valve is adiabatic and the change in kinetic energy is negligible, the temperature of air after throttling will be
A)150 K
B)200 K
C)300 K
D)450 K
E)600 K
A)150 K
B)200 K
C)300 K
D)450 K
E)600 K
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18
Saturated liquid water at 1.0 MPa is throttled adiabatically to a pressure of 0.4 MPa. If the change in kinetic energy is negligible, the percentage of water that evaporates during this throttling process will be
A)0.0%
B)3.8%
C)24.8%
D)7.4%
E)100%
A)0.0%
B)3.8%
C)24.8%
D)7.4%
E)100%
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19
Saturated Refrigerant-134a liquid at 0.8 MPa is throttled to a pressure of 0.12 MPa. The temperature of the refrigerant after throttling is
A)-14.6°C
B)-5.6°C
C)0°C
D)31.3°C
E)-22.4°C
A)-14.6°C
B)-5.6°C
C)0°C
D)31.3°C
E)-22.4°C
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20
Steam at 4 MPa and 400°C is throttled adiabatically to a pressure of 1 MPa. If the change in kinetic energy is negligible, the specific volume of the steam after throttling will be
A)0.2952 m3/kg
B)0.2327 m3/kg
C)0.3749 m3/kg
D)0.5165 m3/kg
E)0.3066 m3/kg
A)0.2952 m3/kg
B)0.2327 m3/kg
C)0.3749 m3/kg
D)0.5165 m3/kg
E)0.3066 m3/kg
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