Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
9th Edition
ISBN: 9781259822674
Author: Yunus A. Cengel Dr., Michael A. Boles
Publisher: McGraw-Hill Education
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Chapter 3.8, Problem 42P

10 kg of R-134a at 300 kPa fills a rigid container whose volume is 14 L. Determine the temperature and total enthalpy in the container. The container is now heated until the pressure is 600 kPa. Determine the temperature and total enthalpy when the heating is completed.

FIGURE P3–42

Chapter 3.8, Problem 42P, 10 kg of R-134a at 300 kPa fills a rigid container whose volume is 14 L. Determine the temperature

Expert Solution & Answer
Check Mark
To determine

The temperature and total enthalpy at initial and final states in the container.

The temperature and total enthalpy at initial and final states when the heating is completed.

Answer to Problem 42P

The temperature and total enthalpy at initial and final states in the container are 0.61°C_ and 545.6kJ_ respectively.

The temperature and total enthalpy at initial and final states when the heating is completed are are 21.55°C_ and 846.4kJ_ respectively.

Explanation of Solution

Since the process is a constant volume, calculate the specific volume.

v1=v2=νm (I)

Here, specific volume at states 1 and 2 are v1andv2 respectively, volume of a rigid container is ν, and mass of a refrigerant R-134a is m.

The initial state represents the mixture, so temperature to be considered as the saturation temperature at given pressure.

Calculate the dryness fraction at state 1.

x1=v1vfvgvf (II)

Here, specific volume at state 1 is v1, specific volume at saturated water is vf, and specific volume at saturated vapor is vg.

Calculate the specific enthalpy at state 1.

h1=hf+x1(hfg) (III)

Here, specific enthalpy at saturated liquid is hf and specific enthalpy at evaporation is hfg.

Calculate the total enthalpy at state 1.

H1=mh1 (IV)

Here, mass of the refrigerant R-134a is m.

Similarly, calculate for x2, h2, and H2 respectively.

x2=v2vfvgvf (V)

Here, dryness fraction at state 2 is x2 and specific volume at state 2 is v2.

Calculate the specific enthalpy at state 2.

h2=hf+x2(hfg) (VI)

Calculate the total enthalpy at state 2.

H2=mh2 (VII)

Conclusion:

Substitute 14 L for ν and 10 kg for m in Equation (I).

v1=14L10kg=14L10kg(1m31000L)=0.0014m3/kg

Write the formula of interpolation method of two variables.

y2=(x2x1)(y3y1)(x3x1)+y1 (VIII)

Here, the variables denote by x and y are pressure and temperature.

Refer to Table A-12, obtain the values of below variables as in Table (I).

Pressure, kPa (x)Temperature, °C (y)
280–1.25
300?
3202.46

Substitute 280 for x1, 300 for x2, 320 for x3, –1.25 for y1, and 2.46 for y3 in Equation (VIII).

y2=(300280)(2.46(1.25))(320280)+(1.25)=0.605

Thus, the value obtained for saturation temperature at the given pressure is 0.605°C.

T1=0.605°C0.65°C

Similarly, calculate the values of vf, vg, hf, and hfg using interpolation method at pressure of 300 kPa as 0.0007735m3/kg, 0.067776m3/kg, 52.71kJ/kg, and 198.17 kJ/kg respectively.

Substitute 0.0014m3/kg for v1, 0.0007735m3/kg for vf, and 0.067776m3/kg for vg in Equation (II).

x1=0.0014m3/kg0.0007735m3/kg0.067776m3/kg0.0007735m3/kg=0.009351

Substitute 52.71kJ/kg for hf, 0.009351 for x1, and 198.17 kJ/kg for hfg in Equation (III).

h1=52.71kJ/kg+(0.009351)(198.17kJ/kg)=54.56kJ/kg

Substitute 10 kg for m and 54.56 kJ/kg for h1 in equation (IV).

H1=10kg(54.56kJ/kg)=545.6kJ

Thus, the temperature and total enthalpy at initial and final states in the container are 0.61°C_ and 545.6kJ_ respectively.

Similarly, calculate the values of vf, vg, hf, and hfg using interpolation method at pressure of 300 kPa as 0.0008198m3/kg, 0.034335m3/kg, 81.50kJ/kg, and 180.95kJ/kg respectively.

Repeat the above steps for T2,x2,h2,andH2 by substituting the values of vf, vg, hf, and hfg in equations (V), (VI), and (VII).

T2=21.55°Cx2=0.01731h2=84.64kJ/kgH2=846.4kJ

Thus, the temperature and total enthalpy at initial and final states in the container are 21.55°C_ and 846.4kJ_ respectively.

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Chapter 3 Solutions

Thermodynamics: An Engineering Approach

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