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Chemical and Mechanical Engineering 2300 / Thermodynamics I 
Solution to Homework Assignment 4 (Lectures 1 - 9) 
Prof. Geoff Silcox 
Chemical Engineering 
University of Utah 
Due Monday, 2014 September 29, by 17:00 
To ensure that you receive full credit for your solutions, write out all equations in 
symbolic form, give numerical values for all variables and constants in the equations, and 
write answers to definitions or conceptual problems in complete sentences. Approximate 
answers are rounded to one significant figure. Your answers need to be reported with 
three. 
Problem 1 
The properties of compressed liquids are commonly approximated by the equation, 
written here for specific volume, 
v(T ,P )  vf (T ) 
Enthalpy (h = u + Pv) is one property where this approximation can lead to significant 
errors because pressure appears explicitly in its definition. Two possible approximations 
for the enthalpy of compressed water are 
 
h(T ,P ) h (T ) 
  
f 
   
h(T,P) h (T ) v (T ) P P (T ) 
f f sat 
The latter is a more accurate approximation than the former. Calculate h at 20C and 100 
bar using these two approximations and compare your answers to that from Table A-7. 
Solution 
From Table A-4 at 20C, h = hf = 83.915 kJ/kg. From the more accurate approximation, 
kJ m3 kJ 83 915 0 001002 10000 2 3392 kPa 93 92 
    
f f sat kg kg kg h  h  v P P  .  .  .  . 
From Table A-7 at 20C and 10 MPa, h = 93.28 kJ/kg. We conclude that the second 
approximation is quite accurate while the first is low by more than 10%. 
Problem 2 
Complete the following table for water.
T, C P, kPa v, m3/kg Phase 
description 
140 0.05 
550 saturated liquid 
125 750 
500 0.140 
Solution 
T, C P, kPa v, m3/kg Phase 
description 
140 361.53 0.05 sat. mixture 
Tsat = 155.46 550 0.001097 saturated liquid 
125 750 0.001065a compres. liq. 
500 2500 0.140 superheated 
Notes 
v = vf at 125C 
Problem 3 
Complete the following table for water. 
T, C P, kPa u, kJ/kg Phase 
description 
400 1450 
220 saturated vapor 
190 2500 
4000 3040 
Solution 
T, C P, kPa u, kJ/kg Phase 
description 
143.61 400 1450 sat. mixture 
220 2319.6 2601.3 sat. vapor 
190 2500 uf = 806.00 compres. liq. 
466.2a 4000 3040 superheated 
Notes 
a) Linear interpolation. 450 500 450 3040 3011 466.2 
3100.3 3011.0 
T 
 
    

Problem 4 
A 0.5-m3 rigid tank contains refrigerant-134a initially at 160 kPa and 40 percent quality. 
Heat is now transferred to the refrigerant until the pressure reaches 700 kPa. Determine 
(a) the mass of the refrigerant in the tank and (b) the amount of heat transferred. Sketch 
the process on a P-v diagram with respect to saturation lines. Approximate answers: the 
mass is roughly 10 kg and Qin is about 3000 kJ. 
Solution 
a) From Table A-12, the constant specific volume for this process is 
m3 1 0.6 0.0007437 0.4 0.12348 0.04984 
      
f g kg v   x v  xv    
The mass of the system is 
3 
0.5 m 10.03 kg 
0.04984m 
   
3 
kg 
m V 
v 
Because we will need it later, u1 is given by 
m3 1 0.6 31.09 0.4 221.35 107.2 
      
f g kg u   x u  xu    
b) Because v2 = 0.04984 m3/kg and P2 = 700 kPa, the final state is superheated vapor. To 
determine the heat added, an energy balance on the system gives 
  2 1 and in out in in U Q W Q Q  m u  u 
Interpolation in Table A-13, slightly outside the bounds, gives u2 = 376.8 kJ/kg and 
finally 
    2 1 10.03 376.8 107.2 2705 in Q  m u  u    kJ 
The process is sketched below on a P-v diagram.
P 
2 
Problem 5 
The Rankine cycle is sketched below. We will discuss this cycle in Lesson 22 of the 
online notes. The cycle is primarily used to generate electricity (the generator is attached 
to the turbine and is not shown here). The working fluid for fossil-fuel-fired and nuclear 
powered systems is water. For lower temperature cycles, the working fluid is commonly 
propane. In the figure below, state 1 is a superheated vapor, state 2 is typically a 
superheated vapor or saturated mixture of high quality, state 3 is a saturated liquid, and 
state 4 is a compressed liquid. 
If the temperature and pressure of the propane at point 1 in the cycle are 220C and 110 
bar(a), calculate the specific volume (m3/kg) by the following techniques. 
a) The ideal gas equation of state (EOS). 
b) The compressibility factor obtained from the Nelson-Obert generalized 
compressibility chart, Figure A-15 of the text. 
c) The Redlich-Kwong EOS, where 
v 
1 
Boiler Turbine 
Pump Condenser 
out , T W 
out Q 
in Q 
in , P W 
Boundary 
of system 
2 
3 
4 
1
3 2  2  
2 
2 25 
0 5 
2 2 
or 0 
where 
0 42748 
0 08664 
. 
C 
. 
C 
C 
C 
Z Pv 
RT 
P RT a Z Z A B B Z AB 
v b v bv 
R T 
a . 
P T 
RT 
b . 
P 
A aP 
R T 
B bP 
RT 
 
        
  
 
 
 
 
Include a plot of the cubic equation, g(Z )  Z3  Z2  A  B  B2 Z  AB , as part 
of your answer. Also include your values of a, b, A, and B, with units as appropriate. 
d) The NIST website, http://webbook.nist.gov/chemistry/fluid/. 
Approximate answers: (a) 0.008 m3/kg, (b) 0.006 m3/kg. 
Solution 
(a) For the ideal gas EOS, 
3 
8 31446 kPa-m 493 15 K kmol-K 008453m 
3 
0 44 097 kg 11000 kPa kg 
. . v  RT   
. 
kmol 
P . 
(b) For the compressibility chart, 
493 15 K 1 334 and 110 bar(a) 2 589 
T  T  .  . P  P   
. 
R T 369 . 8 K R P 42 . 
49 bar(a) 
c c 
and 
 3 
 
  
3 
0 68 8 31446 kPa-m 493 15 K 
. . . 
kmol-K m 0 68 and 0 005748 
Z  . v  ZRT     
. 
44 097 kg 11000 kPa kg 
kmol 
P .
(c) From the Redlich-Kwong EOS, the following values are obtained 
Variable Value 
a 8.236x10-4 kJ-m3/mol 
b 6.269x10-5 m3 
A 0.5389 
B 0.1682 
Z 0.6950 
v 0.005875 m3/kg 
The value of Z = 0.6950 agrees with the plot of g(Z) versus Z. 
0.50 
0.40 
0.30 
0.20 
0.10 
0.00 
‐0.10 
‐0.20 
0.00 0.20 0.40 0.60 0.80 1.00 1.20 
g(Z) 
Compressibility Factor, Z 
The plot was drawn in Excel. The roots of the equation for Z were obtained with the 
MATLAB function “roots” and verified by an iterative solution in Excel using Newtons 
method. 
(d) From the NIST website at 493.15 K and 110 bar(a), v = 0.005996 m3/kg. The NIST 
properties are calculated with a much more sophisticated model than the Redlich-Quong 
EOS. References to the models used are available at 
http://webbook.nist.gov/chemistry/fluid/. In summary, the four methods give the 
following values for v.
Method Specific volume, m3/kg 
Ideal gas EOS 0.00845 
Chart 0.00575 
Redlich-Quong EOS 0.00588 
NIST property calculator 0.00600 
Those from NIST can be considered the most accurate. 
Problem 6 
Steam in a piston-cylinder device expands adiabatically from 700C and 2.0 MPa to 
300C and 0.5 MPa. How much work is done by the steam? Approximate answer: 700 
kJ/kg 
Solution

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Thermodynamics Hw#4

  • 1. Chemical and Mechanical Engineering 2300 / Thermodynamics I Solution to Homework Assignment 4 (Lectures 1 - 9) Prof. Geoff Silcox Chemical Engineering University of Utah Due Monday, 2014 September 29, by 17:00 To ensure that you receive full credit for your solutions, write out all equations in symbolic form, give numerical values for all variables and constants in the equations, and write answers to definitions or conceptual problems in complete sentences. Approximate answers are rounded to one significant figure. Your answers need to be reported with three. Problem 1 The properties of compressed liquids are commonly approximated by the equation, written here for specific volume, v(T ,P )  vf (T ) Enthalpy (h = u + Pv) is one property where this approximation can lead to significant errors because pressure appears explicitly in its definition. Two possible approximations for the enthalpy of compressed water are  h(T ,P ) h (T )   f    h(T,P) h (T ) v (T ) P P (T ) f f sat The latter is a more accurate approximation than the former. Calculate h at 20C and 100 bar using these two approximations and compare your answers to that from Table A-7. Solution From Table A-4 at 20C, h = hf = 83.915 kJ/kg. From the more accurate approximation, kJ m3 kJ 83 915 0 001002 10000 2 3392 kPa 93 92     f f sat kg kg kg h  h  v P P  .  .  .  . From Table A-7 at 20C and 10 MPa, h = 93.28 kJ/kg. We conclude that the second approximation is quite accurate while the first is low by more than 10%. Problem 2 Complete the following table for water.
  • 2. T, C P, kPa v, m3/kg Phase description 140 0.05 550 saturated liquid 125 750 500 0.140 Solution T, C P, kPa v, m3/kg Phase description 140 361.53 0.05 sat. mixture Tsat = 155.46 550 0.001097 saturated liquid 125 750 0.001065a compres. liq. 500 2500 0.140 superheated Notes v = vf at 125C Problem 3 Complete the following table for water. T, C P, kPa u, kJ/kg Phase description 400 1450 220 saturated vapor 190 2500 4000 3040 Solution T, C P, kPa u, kJ/kg Phase description 143.61 400 1450 sat. mixture 220 2319.6 2601.3 sat. vapor 190 2500 uf = 806.00 compres. liq. 466.2a 4000 3040 superheated Notes a) Linear interpolation. 450 500 450 3040 3011 466.2 3100.3 3011.0 T      
  • 3. Problem 4 A 0.5-m3 rigid tank contains refrigerant-134a initially at 160 kPa and 40 percent quality. Heat is now transferred to the refrigerant until the pressure reaches 700 kPa. Determine (a) the mass of the refrigerant in the tank and (b) the amount of heat transferred. Sketch the process on a P-v diagram with respect to saturation lines. Approximate answers: the mass is roughly 10 kg and Qin is about 3000 kJ. Solution a) From Table A-12, the constant specific volume for this process is m3 1 0.6 0.0007437 0.4 0.12348 0.04984       f g kg v   x v  xv    The mass of the system is 3 0.5 m 10.03 kg 0.04984m    3 kg m V v Because we will need it later, u1 is given by m3 1 0.6 31.09 0.4 221.35 107.2       f g kg u   x u  xu    b) Because v2 = 0.04984 m3/kg and P2 = 700 kPa, the final state is superheated vapor. To determine the heat added, an energy balance on the system gives   2 1 and in out in in U Q W Q Q  m u  u Interpolation in Table A-13, slightly outside the bounds, gives u2 = 376.8 kJ/kg and finally     2 1 10.03 376.8 107.2 2705 in Q  m u  u    kJ The process is sketched below on a P-v diagram.
  • 4. P 2 Problem 5 The Rankine cycle is sketched below. We will discuss this cycle in Lesson 22 of the online notes. The cycle is primarily used to generate electricity (the generator is attached to the turbine and is not shown here). The working fluid for fossil-fuel-fired and nuclear powered systems is water. For lower temperature cycles, the working fluid is commonly propane. In the figure below, state 1 is a superheated vapor, state 2 is typically a superheated vapor or saturated mixture of high quality, state 3 is a saturated liquid, and state 4 is a compressed liquid. If the temperature and pressure of the propane at point 1 in the cycle are 220C and 110 bar(a), calculate the specific volume (m3/kg) by the following techniques. a) The ideal gas equation of state (EOS). b) The compressibility factor obtained from the Nelson-Obert generalized compressibility chart, Figure A-15 of the text. c) The Redlich-Kwong EOS, where v 1 Boiler Turbine Pump Condenser out , T W out Q in Q in , P W Boundary of system 2 3 4 1
  • 5. 3 2  2  2 2 25 0 5 2 2 or 0 where 0 42748 0 08664 . C . C C C Z Pv RT P RT a Z Z A B B Z AB v b v bv R T a . P T RT b . P A aP R T B bP RT                Include a plot of the cubic equation, g(Z )  Z3  Z2  A  B  B2 Z  AB , as part of your answer. Also include your values of a, b, A, and B, with units as appropriate. d) The NIST website, http://webbook.nist.gov/chemistry/fluid/. Approximate answers: (a) 0.008 m3/kg, (b) 0.006 m3/kg. Solution (a) For the ideal gas EOS, 3 8 31446 kPa-m 493 15 K kmol-K 008453m 3 0 44 097 kg 11000 kPa kg . . v  RT   . kmol P . (b) For the compressibility chart, 493 15 K 1 334 and 110 bar(a) 2 589 T  T  .  . P  P   . R T 369 . 8 K R P 42 . 49 bar(a) c c and  3    3 0 68 8 31446 kPa-m 493 15 K . . . kmol-K m 0 68 and 0 005748 Z  . v  ZRT     . 44 097 kg 11000 kPa kg kmol P .
  • 6. (c) From the Redlich-Kwong EOS, the following values are obtained Variable Value a 8.236x10-4 kJ-m3/mol b 6.269x10-5 m3 A 0.5389 B 0.1682 Z 0.6950 v 0.005875 m3/kg The value of Z = 0.6950 agrees with the plot of g(Z) versus Z. 0.50 0.40 0.30 0.20 0.10 0.00 ‐0.10 ‐0.20 0.00 0.20 0.40 0.60 0.80 1.00 1.20 g(Z) Compressibility Factor, Z The plot was drawn in Excel. The roots of the equation for Z were obtained with the MATLAB function “roots” and verified by an iterative solution in Excel using Newtons method. (d) From the NIST website at 493.15 K and 110 bar(a), v = 0.005996 m3/kg. The NIST properties are calculated with a much more sophisticated model than the Redlich-Quong EOS. References to the models used are available at http://webbook.nist.gov/chemistry/fluid/. In summary, the four methods give the following values for v.
  • 7. Method Specific volume, m3/kg Ideal gas EOS 0.00845 Chart 0.00575 Redlich-Quong EOS 0.00588 NIST property calculator 0.00600 Those from NIST can be considered the most accurate. Problem 6 Steam in a piston-cylinder device expands adiabatically from 700C and 2.0 MPa to 300C and 0.5 MPa. How much work is done by the steam? Approximate answer: 700 kJ/kg Solution