Chapter 3
Short Description
thermodynamics chapter 3rd that a good solution...
Description
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Chapter 3 Problems Problem 3.1: Express the volume expansivity β and isothermal compressibility κ as functions of density ρ and its partial derivatives. The isothermal compressibility coefficient () of water at 50 oC and 1 bar is
−6
44.18∗10
bar-1. To what pressure must water be compressed at 50 oC to change its density by 1%? Assume that is independent of P. Given Data:
Volume expansivity=β=
1 ∂V V ∂T
( )
P
Or β=
1 dV V dT
( ) →(1) P
Isothermal Compressibilty=κ=
−1 ∂ V V ∂P
( )
T
Or κ=
−1 dV V dP
( ) → ( 2) T
Temperature=T =50 Pressure=P1=1 ¯¿
¿¯ κ=44.18∗10−6 ¿ −1
(a)
1
We know that
C
Density of water =ρ1=1 P2=?
Solution:
0
kg m3
ρ2=( 1+1 )
kg m3
ρ2=1.01
kg m3
August 20, 2013
ρ=
1 V
PROBLEMS
V=
ZAID YAHYA
11-CH-74
1 ρ
Put in (1) & (2)
β=ρ
( dTd 1ρ )
β= P
−ρ dρ 2 ρ dT
( )
β=
P
−1 dρ ρ dT
( ) Proved P
Now, κ=−ρ
(
d 1 dP ρ
)
κ=
T
ρ dρ ρ2 dP
( )
T
κ=
1 dρ ρ dP
( ) Proved T
(b)
As κ=
1 dρ ρ dP
( )
κdP=
T
dρ ρ
Integrating on both sides P2
ρ2
κ ∫ dP=∫ P1
ρ1
dρ ρ
P2
ρ2
1
1
κ|P|P =|ln ρ|ρ
κ ( P2 −P 1 )=( ln ρ 2−ln ρ1 )
κ ( P2 −P 1 )=ln
ρ2 ρ1
Putting values ¯¿ ( P2−1 )= ln1.01 1 −6 44.18∗10 ¿
¯¿ −6 44.18∗10 P2−1=0.00995∗¿
P2=( 225.22+1 ) ¯¿
P2=226.22 ¯¿
Answer
Problem 3.2: Generally, volume expansivity β and isothermal compressibility κ depend on T and P. Prove that
( ∂∂ Pβ ) =−( ∂T∂κ ) T
2
P
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Solution:
We know that Volume expansivity=β=
Since
β
1 ∂V V ∂T
( )
P
is very small V=
1 ∂V ∂ β ∂T
( ) → (1)
Isothermal Compressibilty=κ=
P
−1 ∂ V V ∂P
( )
T
Since κ is very small V=
−1 ∂ V ∂κ ∂ P
1 ∂V ∂β ∂T
∂V ( ) =−1 ∂κ ( ∂ P)
( )
T
P
1 1 ∂ β ∂T
1 ∂V ( ) ∂V =−1 ∂κ (∂P)
T
P
T
( ∂T∂ κ ) =( ∂∂ Pβ )
−
P
T
( ∂∂ Pβ ) =−( ∂T∂κ ) Proved T
P
Problem 3.3: The Tait equation for liquids is written for an isotherm as: AP V =V 0 1− B+ P
(
)
Where V is specific or molar volume, Vo is the hypothetical molar or specific volume at P = 0 and A & B are positive constant. Find an expression for the isothermal compressibility consistent with this equation.
Solution:
We Know That, Isothermal Compressibilty=κ=
3
−1 ∂ V V ∂P
( ) → (1) T
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Given that
(
V =V 0 1−
AP B+ P
)
Where V0 = Hypothetical molar/specific volume at zero pressure, so it is constant V = Molar/specific volume Now, AP V =V o − V B+ P o V −V o =
−AP V B+ P o
V −V o −AP = Vo B+ P
Differentiate w.r.t Pressure 1 ∂ −∂ AP ( V −V o ) = ∂ P B + P V o ∂P
(
−1 ∂V AB+ AP− AP = Vo ∂ P ( B+ P )2
( )
)
[
A ( B+ P )− AP ( 1 ) 1 ∂V −0 =− V o ∂P ( B+ P )2
(
)
]
−1 ∂V AB = V o ∂ P ( B+ P )2
( )
Since, Temperature is constant Therefore, −1 ∂V AB = V o ∂ P T ( B+P )2
( )
Or, From (1)
κ=
AB Proved ( B+ P )2
Problem 3.4: For liquid water the isothermal compressibility is given by: c κ= V ( P+b ) Where c & b are functions of temperature only if 1 kg of water is compressed isothermally & reversibly from 1 bar to 500 bars at 60 oC, how much work is required? At 60 oC, b=2700 bars and c = 0.125 cm3 g-1 4
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Given Data:
Isothermal compressibility=κ=
c V ( P+ b )
Pressure=P1=1 ¯¿
Mass of water=m=1 kg
P2=500 bars Temperature=T =60 c=0.125 cm3 / g
b=2700 bars
Work=W =?
0
C
Solution:
We know that W =−∫ PdV →(1)
κ=
c →(2) V ( P+b )
Also κ=
−1 dV V dP
( ) → ( 3) T
Comparing (2) & (3) −1 dV c = V dP V ( P+b )
−dV =
c dP P+b
Put in (1) c dP W =−∫−P P+b P2
P2
W =c ∫ dP−b c ∫ P1
P1
P2
P W =c ∫ dP P+b P
1 dP P+b
1
P2
P+b−b W =c ∫ dP P+ b P
P2
P2
1
1
[
W =c ( P2 −P 1) −bc ln
Putting values 5
P2
1
1
P+b b W =c ∫ dP−c ∫ dP P+b P+ b P P
1
W =c|P|P −bc|ln (P+b)|P
P2
W =c ( P2 −P 1) −bc [ ln ( P2 +b ) −ln ( P1 +b ) ] P2 +b P1 +b
]
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74 3
3
cm ∗¯¿ g 3 ¯ cm ∗¿ −57.216 ¿ g W =62.375 ¿
3
cm ( ¯ ¯¿ 0.125 cm ∗ln 500+ 2700 W =0.125 ∗ 500−1 )−2700 g g 1+2700
3
cm ∗¯¿ g W =5.16¿
3
cm ∗¯¿ ∗1 m3 g ∗101325 N 1003 cm 3 ∗J 1.01325 ¯¿ m2 Nm W =5.16 ¿
W =0.516
J Answer g
Problem 3.5: Calculate the reversible work done in compressing 1 ft 3 of mercury at a constant temperature of 32F from 1(atm) to 3,000(atm). The isothermal compressibility of mercury at 32F is: κ/(atm)-1 = 3.9 x 10-6 - 0.1 x10-9P(atm) Given Data:
Work done=W =?
Volume=V =1 ft 3
Pressure=P2=3000 atm
Temperature=T =32 F
Pressure=P1=1 atm
κ /atm−1=3.9∗10−6−0.1∗10−9 P (atm)
Where Term,
3.9*10-6
has
unit
of
atm-1
&
Solution:
We know that, work done for a reversible process is
W =−∫ PdV →(1) Also κ=
6
−1 dV V dP
( )
T
dV =−κVdP
0.1*10-9
has
units
of
atm-2
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Put in (1), P2
W =−∫ P (−κVdp )
W =V ∫ κ P dP P1
P2
P2
−6 −9 W =V ∫ ( 3.9∗10 −0.1∗10 P ) P dP
3000
W =3.9∗10 V
∫
P dP−0.1∗10 V
P1
∫
P2 dP
1
3000
||
P2 W =3.9∗10 V 2 W=
P1
−9
3000 −9
1
−6
2
W =V ∫ 3.9∗10 P dP−V ∫ 0.1∗10 P dP
P1
−6
P2 −6
1
3000
||
P3 −0 .1∗10 V 3 −9
1
1.95∗10−6∗1 ft 3 ( 3.333∗10−11∗1 ft 3 ( 30002−12 ) atm2− ∗ 30003−13 ) atm3 2 atm atm
W = (17.55−0.8991 ) atm∗ft 3
W =16.65atm∗ft 3 Answer
Problem 3.6: Five kilograms of liquid carbon tetrachloride undergo a mechanically reversible, isobaric change of state at 1 bar during which the temperature change from 0 oC to 20oC. Determine ΔVt, W, Q, and ΔUt. The properties for liquid carbon tetrachloride at 1 bar & 0 oC may be assumed independent of temperature: β = 1.2 x 10-3 K-1 Cp = 0.84 kJ kg-1 K-1, ρ = 1590 kg m-3 Given Data:
Mass=m=5 kg
Pressure=P=1 ¯ ¿
T 1 =273.15 K
7
Temperature=T 1=0
0
C
August 20, 2013
PROBLEMS
ZAID YAHYA
Temperature=T 2=20 T 2 =( 20+273.15 ) K
T 2 =293.15 K
−3
β=1.2∗10 K
0
C
C P=0.84
−1
11-CH-74
kJ kg∗K
ρ=1590
kg m3
t
Q=?
∆ U =?
Solution:
As V=
1 ρ
V 1=
1 ρ1
1 m3 V 1= 1590 kg
Also, we know that Volume expansivity=β=
1 dV V dT
( )
βdT =
P
1 dV V
Integrating on both sides, T2
V2
β ∫ dT =∫ T1
V1
dV V
T2
V2
1
1
β|T |T =|lnV |V
β ( T 2−T 1 )=( lnV 2−ln V 1 )
β ( T 2−T 1 )=ln
V2 V1
Putting values V ∗1590 kg 1.2∗10 ∗( 293.15−273.15 ) K =ln 2 K m3 −3
V 2=0.000644
e
0.024
=
V 2∗1590 kg m3
m3 kg
Now, ∆ V =V 2−V 1
(
∆ V = 0.000644−
Now, for total volume,
8
1 m3 1590 kg
)
∆ V =15.28∗10−6
3
m kg
t
∆ V =?
1.024 ∗m3 1590 V 2= kg
W =?
August 20, 2013
PROBLEMS
∆ V t =∆ V ∗m
ZAID YAHYA
∆ V t =( 15.28∗10−6∗5 )
m3 ∗kg kg
11-CH-74
∆ V t =7.638∗10−5 m3 Answer
Now, We know that for a reversible process,
Work done=W =−P ∆ V t W =−1 ¯¿ 7.638∗10−5
m3∗101325 N ∗J 1.01325 ¯¿ m2 ∗1 kJ Nm 1000 J
W =−7.638∗10−3 kJ Answer
Now, For a reversible process at constant pressure,we have Q=∆ H
Q=m C P ∆ T
Q=5 kg∗0.84
kJ ∗( 293.15−273.15 ) K kg∗K
Q=84 kJ Answer
Now, According to first law of thermodynamics, ∆ U t =Q+W
∆ U t =( 84−7.368∗10−3 ) kJ
∆ U t =83.99 kJ Answer
Problem 3.7: A substance for which k is a constant undergoes an isothermal, mechanically reversible process from initial state (P1, V1) to (P2, V2), where V is a molar volume. a) Starting with the definition of k, show that the path of the process is described by V = A ( T ) exp (−κP) b) Determine an exact expression which gives the isothermal work done on 1 mol of this constant-k substance.
Solution: (a)
We know that
Isothermal compressibilty =κ= Integrating on both sides,
9
−1 dV V dP
( )
T
dV =−κdP V
August 20, 2013
∫
PROBLEMS
ZAID YAHYA
dV =−κ ∫ dP V
lnV =−κP+lnA ( T ) Where ln A (T) is constant of integration & A depends on T only
lnV −lnAT =−κP
ln
V =−κP A (T )
Taking anti log on both sides,
V =e−κP AT
V = A ( T ) e−κP
Or
V = A ( T ) exp (−κP ) Proved
(b)
Work done=W=?
For a mechanically reversible process, we have,
dW =−PdV → ( 1 ) Using,
d ( PV ) =PdV +VdP
−PdV =VdP −d ( PV )
Put in (1)
dW =VdP−d ( PV ) → ( 2 )
We know that
Isothermal compressibilty =κ= Put in (2)
dW =
−dV −d ( PV ) κ
Integrating on both sides,
10
−1 dV V dP
( )
T
−dV =VdP κ
11-CH-74
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
−1
∫ dW = κ ∫ dV −∫ d ( PV ) W=
−1 Δ V −Δ ( PV ) κ
Since volume changes from V1 to V2 & pressure changes from P1 to P2 , Therefore,
W=
−1 ( V 2−V 1 ) −( P2 V 2−P1 V 1 ) κ
W=
( V 1−V 2 ) κ
+ P1 V 1−P2 V 2 Proved
Problem 3.8: One mole of an ideal gas with C V = 5/2 R, CP = 7/2 R expands from P 1 = 8 bars & T1= 600 K to P2 = 1 bar by each of the following path: a) Constant volume b) Constant temperature c) Adiabatically Assuming mechanical reversibility, calculate W, Q, ∆ U, and ∆ H for each of the three processes. Sketch each path in a single PV diagram. Given Data:
5 CV = R 2
7 C P= R 2
P1=8 ¯¿
T 1 =600 K
Solution: (a)
According to first law of thermodynamics,
∆ U =Q+W →(1) For a constant volume process,
W =0
∆ U =CV ∆T
Put in (1)
Q=∆U =C V ∆ T
11
Q=∆U =C V ( T 2 −T 1 ) →(2)
P2=1 ¯¿
W =?
Q=?
∆ U =?
∆ H=?
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
For T2 , We know that for an ideal gas
T1 T 2 = P1 P2
T2=
T1 ∗P P1 2
8 ¯¿∗1 ¯¿ 600 K T2= ¿
T 2 =75 K
Put in (2),
5 Q=∆U = R ( 75−600 ) K 2
Q=∆U =
−5 J ∗8.314 ∗525 K 2 mol∗K
Q=∆U =−10.912
Q=∆U =−10912
kJ Answer mol
Also For a mechanically reversible process we have,
∆ H=C P ∆ T
7 ∆ H= R ( T 2−T 1 ) 2
7 J ∆ H= ∗8.314 ∗( 75−600 ) K 2 mol∗K ∆ H=−15.277
∆ H=−15277
kJ Answer mol
(b)
For a constant temperature process,
∆ U =0
∆ H=0
We know that at constant temperature, work done is
W =R T 1 ln W =8.314
J 1 ∗600 K∗ln mol∗K 8
0=Q+ W
Q=−W
Or
Q=10.373
kJ Answer mol
(c)
12
We know that for an adiabatic process
P2 P1
W =−10373
Now, according to first law of thermodynamics,
∆ U =Q+W
J mol
J mol
W =−10.373
kJ Answer mol
J mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Q=0 Now, according to first law of thermodynamics,
∆ U =Q+W
∆ U =W →(1)
∆ U =CV ∆T Put in (1)
W =∆ U=C V ∆ T
W =∆ U=C V ( T 2−T 1 ) →(2)
For T2 , We know that for an adiabatic process
T1 P
( 1−γ ) γ 1
=T 2 P
( 1−γ ) γ 2
T 2 =T 1
P1 P2
( )
( 1−γ ) γ
T 2 =600 K
8 1
()
( 1−1.4 ) 1.4
T 2 =331.23 K
Put in (2)
5 W =∆ U= R∗( 331.23−600 ) K 2
W =∆ U=
−5 J ∗8.314 ∗268.77 K 2 mol∗K
W =∆ U=5.5864
W =∆ U=−5586.4
J mol
J Answer mol
For a mechanically reversible adiabatic process we have
7 ∆ H= R ( T 2−T 1 ) 2
∆ H=C P ∆ T ∆ H=−7.821
7 J ∆ H= ∗8.314 ∗( 331.23−600 ) K 2 mol∗K
J Answer mol
Problem 3.9: An ideal gas initially at 600k and 10 bar undergoes a four-step mechanically reversible cycle in a closed system. In step 12, pressure decreases isothermally to 3 bars; in step 23, pressure decreases at constant volume to 2 bars; in step 34, volume decreases at constant pressure; and in step 41, the gas returns adiabatically to its initial state. Take CP = (7/2) R and CV = (5/2) R. a) Sketch the cycle on a PV diagram. b) Determine (where unknown) both T and P for states 1, 2, 3, and 4. c) Calculate Q, W, ∆ U, and ∆ H for each step of the cycle. Given Data: 13
August 20, 2013
PROBLEMS
ZAID YAHYA
Initial Temperature=T 1=600 K
Initial Pressure=P1=10 ¯¿
11-CH-74
7 C P= R 2
5 CV = R 2
Solution: (b)
Step 12, an Isothermal process, Since For an isothermal process, temperature is constant Therefore,
T 2 =T 1=600 K
P2=3 ¯¿
We know that, for an ideal gas
P2 V 2 =R T 2
V 2=
RT 2 P2
2 ¯ ¿∗1.01325 ¯ ¿m ∗N∗m 101325 N mol∗K∗3 J 8.314∗J∗600 K V 2= ¿
3
V 2=0.0166
m mol
Step 23, an Isochoric process, Since For an isochoric process, Volume is constant Therefore,
m3 V 3=V 2=0.0166 mol
P3=2 ¯¿
We know that, for an ideal gas
P3 V 3 =RT 3
T3=
P3 V 3 R
2 ¯¿ 0.0166 m 3∗mol∗K ∗J mol∗8.314 J ∗101325 N N∗m T3= 1.01325 ¯¿ m2
Step 34, an Isobaric process, Since For an isobaric process, pressure is constant 14
T 3 =400 K
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Therefore,
P4 =P 3=2 ¯¿ For T4 , we will use an adiabatic relation of temperature and pressure As
T 4 P4 = T1 P1
( )
R CP
T 4=T 1
P4 P1
( )
R CP
2 10
( )
T 4=600 K∗
2∗R 7R
T 4=378.83 K
We know that, for an ideal gas
P4 V 4 =RT 4
V 4=
2 ¯¿∗1.01325 ¯ ¿m ∗Nm 101325 N mol∗K∗2 J 8.314 J∗378.83 K V 4= ¿
RT4 P4
3
V 4 =0.0157
m mol
Step 41, an adiabatic process, Since Gas returns to its initial state adiabatically Therefore,
T 1 =600 K
P1=10 ¯¿
We know that, for an ideal gas
P1 V 1=R T 1
V 1=
RT 1 P1
¯¿∗1.01325 ¯¿ m2 ∗Nm 101325 N mol∗K∗10 J 8.314 J∗600 K V 1= ¿
(c)
Step 12, an Isothermal process, Since For an isothermal process, temperature is constant Therefore
15
V 1=4.988∗10−3
3
m mol
August 20, 2013
∆ U 12 =0
PROBLEMS
11-CH-74
∆ H 12=0
For an isothermal process, we have
Q=−R T 1 ln
ZAID YAHYA
P2 P1
Q=−8.314
J 3 ∗600 K∗ln mol∗K 10
Q=6006
J mol
Q=6.006∗103
J Answer mol
According to first law of thermodynamics
∆ U 12=Q12 +W 12
0=Q12+W 12
W 12=−Q12
W 12=−6.006∗103
J Answer mol
Step 23, an Isochoric process, Since For an isochoric process, Volume is constant Therefore,
W 23=0 At constant volume we have
Q23=∆ U 23=CV ∆ T
Q23=∆ U 23=CV ( T 3−T 2 )
5 ∗8.314 J 2 Q23=∆ U 23= ∗(−200 ) K mol∗K
5 Q23=∆ U 23= R ( 400−600 ) K 2
Q23=∆ U 23=−4157
J mol
Q23=∆ U 23=−4.157∗10 3
J Answer mol
We know that
∆ H 23=C P ∆ T
∆ H 23=C P ( T 3−T 2 )
∆ H 23=−5820
Step 34, an Isobaric process, Since For an isobaric process, pressure is constant Therefore, at constant pressure we have, 16
7 ∆ H 23= R ( 400−600 ) K 2 J mol
∆ H 23=−5.82∗103
7 J ∆ H 23= ∗8.314 ∗(−200 ) K 2 mol∗K J Answer mol
August 20, 2013
PROBLEMS
Q34=∆ H 34 =C P ∆ T
ZAID YAHYA
7 Q34=∆ H 34 = R ( T 4−T 3 ) 2
11-CH-74
7 J Q34=∆ H 34 = ∗8.314 ∗( 378.83−400 ) K 2 mol∗K
Q34=∆ H 34 =−616
J Answer mol
For an Isobaric process we have
W 34=−R ∆ T
W 34=−R ( T 4−T 3 )
W 34=−8.314
J ∗( 378.83−400 ) K mol∗K
W 34=176
J Answer mol
We know that,
∆ U 34 =CV ∆ T
5 ∆ U 34 = R ( T 4 −T 3 ) 2
5 J ∆ U 34 = ∗8.314 ∗( 378.83−400 ) K 2 mol∗K
∆ U 34 =−440
J Answer mol
Step 41, an adiabatic process, Since For an adiabatic process there is no exchange of heat Therefore,
Q41=0 We know that,
∆ U 41=C V ∆ T
5 ∆ U 41= R ( T 1−T 4 ) 2
5 J ∆ U 41= ∗8.314 ∗( 600−378.83 ) K 2 mol∗K
∆ U 41=4.597∗103
∆ U 41=4597
J mol
J Answer mol
We know that
∆ H 41=C P ∆T
7 ∆ H 41= R ( T 1−T 4 ) 2
7 J ∆ H 41= ∗8.314 ∗( 600−378.83 ) K 2 mol∗K
∆ H 41=6.4358∗103
17
According to first law of thermodynamics
J Answer mol
∆ H 41=6435.8
J mol
August 20, 2013
PROBLEMS
ZAID YAHYA
∆ U 41=Q 41+W 41
∆ U 41=W 41
11-CH-74 3
W 41=4.597∗10
J Answer mol
Problem 3.10: t An ideal gas, CP= (5/2) R and CV= (3/2) R is changed from P1 = 1bar and V 1 = 12m3 to P2 = 12 bar and t
V 2 = 1 m3 by the following mechanically reversible processes: a) Isothermal compression b) Adiabatic compression followed by cooling at constant pressure. c) Adiabatic compression followed by cooling at constant volume. d) Heating at constant volume followed by cooling at constant pressure. e) Cooling at constant pressure followed by heating at constant volume. Calculate Q, W, change in U, and change in H for each of these processes, and sketch the paths of all processes on a single PV diagram. Given Data:
5 C P= R 2
3 CV = R 2
V t2=1 m3
Q=?
Initial pressure=P1=1 ¯¿ W =?
∆ H=?
Solution: Since
Temperature=constant Therefore, for all parts of the problem,
∆ H=0
∆ U =0
(a)
Isothermal compression,
For an isothermal process, we have
Q=−R T 1 ln
P2 P1
Since For an ideal gas, we have 18
∆ U =?
t
3
V 1=12 m
Final pressure=P 2=12 ¯¿
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
P1 V 1=R T 1 Therefore,
Q=−P1 V 1 ln
P2 P1
12 ∗101325 N 1 ∗J 2 1.01325 ¯¿ m ∗1 kJ Nm 3 Q=−1 ¯¿ 12 m ∗ln 1000 J
Q=−2981.88 kJ Answer
According to first law of thermodynamics
∆ U =Q+W
0=Q+ W
W =−Q
W 12=2981.88 kJ Answer
(b)
Adiabatic compression followed by cooling at constant pressure Since For an adiabatic process, there is no exchange of heat Therefore,
Q=0 Answer The process completes in two steps First step, an adiabatic compression to final pressure P 2 , intermediate volume can be given as ' γ
P2 ( V ) =P 1 V 1
V ' =V 1
P1 P2
( )
1 γ
For mono atomic gas, we have
γ =1.67
1 12
( )
V ' =12 m3∗
1 1.67
V ' =2.71 m3
We know that, '
P V −P 1 V 1 W 1= 2 γ−1
19
August 20, 2013
PROBLEMS
ZAID YAHYA
( 12∗2.71−1∗12 ) ¯¿ m3 ∗101325 N 1.67−1 ∗J 1.01325 ¯¿ m2 ∗1 kJ Nm W 1= 1000 J
11-CH-74
W 1=3063 kJ →(1)
Second step, cooling at constant pressure P2 We know that, for a mechanically reversible process
m3∗101325 N ∗J 1.01325 ¯¿ m2 ∗1 kJ Nm ¯ W 2=−12 ( 1−2.71 ) 1000 J
W 2=−P2 ( V 2−V ' )
W 2=2052 kJ →( 2)
Now
W =W 1+ W 2
W = ( 3063+ 2052 ) kJ
W =5115kJ Answer
(c)
Adiabatic compression followed by cooling at constant volume Since For an adiabatic process, there is no exchange of heat Therefore,
Q=0 Answer First step, an adiabatic compression to volume V2 , intermediate pressure can be given as '
γ
P V 2 =P1 V 1
V P =P1 1 V2 '
( )
For mono atomic gas, we have
γ =1.67
P' =1
1.67 12¯ 1
( )
We know that,
20
γ
P' =63.42 ¯¿
August 20, 2013
PROBLEMS
'
W 1=
ZAID YAHYA
P V 2−P 1 V 1 γ −1
( 63.42∗1−1∗12 ) ¯¿ m3 ∗101325 N 1.67−1 ∗J 1.01325 ¯¿ m 2 ∗1 kJ Nm W 1= 1000 J
11-CH-74
W 1=7674.76 kJ
Second step, cooling at constant Volume, Therefore, No work will be done
W 2=0 Now
W =W 1+ W 2
W = (7674.76+ 0 ) kJ
W =7674.76 kJ Answer
(d)
Heating at constant volume followed by cooling at constant pressure The process completes in two steps Step 1, Heating at constant volume to P2 Therefore no work will be done
W 1=0 Step 2, Cooling at constant pressure P2 To V2 We know that, for a mechanically reversible process
W 2=−P2 ∆ V
W 2=−P2 ( V 2−V 1 )
m3∗101325 N ∗J 1.01325 ¯¿ m2 ∗1 kJ Nm ¯ W 2=−12 ( 1−12 ) 1000 J
Now
W =W 1+ W 2
W = ( 0+13200 ) kJ
W =13200 kJ Answer
According to first law of thermodynamics
∆ U =Q+W
0=Q+ W
Q=−W
Q=−13200 kJ Answer
(e)
Cooling at constant pressure followed by heating at constant volume 21
W 2=13200 kJ
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
The process completes in two steps Step 1, Cooling at constant Pressure P1 to V2 Therefore, for a mechanically reversible process 3
W 1=−P1 ∆ V
W 1=−P1 ( V 2−V 1 )
m ∗101325 N ∗J 2 1.01325 ¯ ¿m ∗1 kJ Nm ¯ W 1=−1 ( 1−12 ) 1000 J
W 1=1100 kJ
Step 1, Heating at constant Volume V2 to pressure P2 Therefore no work will be done
W 2=0 Now
W =W 1+ W 2
W = (1100 +0 ) kJ
W =1100 kJ Answer
According to first law of thermodynamics
∆ U =Q+W
0=Q+ W
Q=−W
Q=−1100 kJ Answer
Problem 3.11: The environmental lapse rate
dT dz characterizes the local variation of temperature with elevation in the
earth's atmosphere. Atmospheric pressure varies with elevation according to the hydrostatic formula, dP =−M ρg dz Where M is a molar mass, ρ is molar density and g is the local acceleration of gravity. Assume that the atmosphere is an ideal gas, with T related to P by the polytropic formula equation (3.35 c). Develop an expression for the environmental lapse rate in relation to M, g, R, and δ.
Solution: Given that
dP =−M ρg → ( 1 ) dz
22
The polytropic relation is
August 20, 2013
TP
1−δ δ
PROBLEMS
ZAID YAHYA
=Constant
Or
TP
1−δ δ
1−δ
=T o Po δ
Where To =Temperature at sea level, so it is constant Po = Pressure at sea level, so it is constant
T P
δ−1 δ
T To
( )
=
To P
δ δ−1
δ−1 δ o
P = Po
T P = T o Po
( )
δ−1 δ
T P=Po To
( )
δ δ −1
→(a)
P=
Po To
δ δ−1
δ
∗T δ −1
Differentiate w.r.t to Temperature on both sides
Po δ δ −1
Po
∗δ
dP T o = ∗T dT δ−1
1 δ−1
δ δ−1
∗δ
1 To δ−1 dP= ∗T dT →(2) δ−1
We know that, for an ideal gas
ρ=
P RT
Where
R=Specific gas constant=R ' /M
Put (a) in above equation
ρ=
Put in (1) 23
1 T ∗Po RT To
( )
δ δ −1
11-CH-74
August 20, 2013
PROBLEMS
dP g∗1 T =−M Po dz RT To
( )
δ δ −1
ZAID YAHYA
dP=−M
g∗1 T Po RT To
( )
δ δ−1
11-CH-74
∗dz
Put (2) in above
Po δ δ−1
−δ −1 ∗M g δ ∗Po δ R ∗T o δ−1 Po
∗δ
To δ−1
∗T
1 δ −1
dT =−M
g∗1 T P RT o T o
( )
δ δ−1
∗dz
−δ−1 ∗M g δ ∗Po δ R ∗T o δ−1 Po dT = dz
To
δ δ−1
T
To
dT = dz
δ δ−1
T∗T
δ
∗T δ −1
1 δ−1
δ
∗T δ −1
δ δ−1
−δ ∗M g dT δ−1 = Proved dz R
Problem 3.12: An evacuated tank is filled with gas from a constant pressure line. Develop an expression relating the temperature of the gas in the tank to temperature T’ of the gas in line. Assume that gas is ideal with constant heat capacities, and ignore heat transfer between the gas and the tank. Mass and energy balances for this problem are treated in Ex. 2.13.
Solution:
24
Choose the tank as the control volume. There is no work, no heat transfer & kinetic & potential energy changes are assumed negligible. Therefore, applying energy balance
August 20, 2013
PROBLEMS
d ( mU )tank +∆ ( Hm )=0 dt
ZAID YAHYA
d ( mU )tank + H ' ' m' ' −H ' m' =0 dt
Since Tank is filled with gas from an entrance line, but no gas is being escaped out, Therefore,
d ( mU )tank +0−H ' m' =0 dt
d ( mU )tank −H ' m' =0→(1) dt
Where prime (‘) denotes the entrance stream Applying mass balance
m' =
d mtank → ( 2) dt
Combining equation (1) & (2)
d ( mU )tank ' d m tank −H =0 dt dt
1 {d ( mU )tank −H ' d mtank }=0 dt
'
d ( mU )tank =H d mtank
Integrating on both sides m2
m2
∫ d ( mU )tank=H ' ∫ d mtank m1
∆ ( mU )tank =H ' ( m 2−m 1 )
m1
m 2 U 2 −m1 U 1=H ' ( m 2−m 1 ) Because mass in the tank initially is zero, therefore
m1=0 m2 U 2 =H ' m2 '
U 2=H →(3) We know that 25
11-CH-74
August 20, 2013
PROBLEMS
U=C V T
ZAID YAHYA
11-CH-74
U 2=C V T 2 → ( a )
Also
H ' =C P T ' → ( b ) Put (a) & (b) in (3)
CV T =C P T '
T=
CP ' T CV
Since heat capacities are constant, therefore
γ=
CP CV
T =γ T ' Proved
Problem 3.14: A tank of 0.1-m3 volume contains air at 25 oC and 101.33 kPa. The tank is connected to a compressed-air line which supplies air at the constant conditions of 45oC and 1,500 kPa. A valve in the line is cracked so that air flows slowly into the tank until the pressure equals the line pressure. If the process occurs slowly enough that the temperature in the tank remains at 25 oC, how much heat is lost from the tank? Assume air to be an ideal gas for which CP = (7/2) R and CV = (5/2) R Given Data:
Volume=V =0.1 m3 Heat lost =Q=?
T 1 =25 o. C =298 K 7 C P= R 2
P1=101.33 kPa
T 2 =45 o.C =318 K
5 CV = R 2
Solution:
According to first law of thermodynamics
∆ U =Q+W →(1) Since
∆ H=∆ U +∆ ( PV ) 26
∆ U =∆ H−∆ ( PV )
∆ U =∆ H−P ∆ V −V ∆ P→ ( a )
P2=1500 kPa
August 20, 2013
PROBLEMS
ZAID YAHYA
Also, we know that
W =−P ∆ V → ( b ) Put (a) & (b) in (1)
∆ H−P ∆V −V ∆ P=Q−P ∆ V Also, we have
∆ H=nC P ∆T
∆ H=nC P ( T 2−T 1 )
Put in (2)
n C P ( T 2−T 1 )−V ∆ P=Q →(3)
For “n”
We know that for an ideal gas,
PV =nRT Initial number of moles of gas can be obtained as,
P1 V =n1 R T 1
n1=
P1 V RT1
The final number of moles of gas at temperature T1 are
P2 V =n2 R T 1
n2 =
P2 V RT 1
Now, Applying molar balance
n=n1−n 2 Put in (3)
27
n=
P1 V P2 V − R T1 R T1
n=
( P1−P 2) V RT1
∆ H−V ∆ P=Q→ ( 2 )
11-CH-74
August 20, 2013
PROBLEMS
ZAID YAHYA
( P 1−P2 ) V R T1
( P1−P2 ) V C ( T 2−T 1 )−V ∆ P=Q P
( P1−P2 ) V T1 2
RT1 2
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∗7 R∗( T 2−T 1 )−V ∆ P=Q
∗7 ∗( T 2 −T 1 )−V ( P2 −P 1 )=Q
( 101.33−1500 ) kPa∗0.1 m3 ∗7 298 K ∗( 318−298 ) K −0.1 m3 ( 1500−101.33 ) kPa=Q 2 kPa∗1 kN ∗1 kJ 2 3 1 kPa∗m Q=−172.717 m 1 kNm
Q=−172.717 kJ Answer
Problem 3.17: A rigid, no conducting tank with a volume of 4 m 3 is divided into two unequal parts by a thin membrane. One side of the membrane, representing 1/3 of the tank, contains nitrogen gas at 6 bars and 100 oC, and the other side, representing 2/3 of the tank, is evacuated. The membrane ruptures and the gas fills the tank. a) What is the final, temperature of the gas? How much work is done? Is the process reversible? b) Describe a reversible process by which the gas can be returned to its initial state, How much work is done Assume nitrogen is an ideal gas for which CP = (7/2) R & CV = (5/2) R Given Data:
3
Volume of thetank=V 1 =4 m V 3=
V 1∗2 8 3 = m 3 3
Solution:
(a)
Finaltemperature=T 2=? 28
V 2=
V 1∗1 4 3 = m 3 3
Pressure=P2=6 ¯¿
o
Temperature=T 1=100 . C
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
According to first law of thermodynamics
∆ U =Q+W Since No work is done & no heat is transferred Therefore
Q=W =0
mC V ∆ T =0
∆ U =0
∆ T =0
T 2 −T 1=0
T 2 =T 1
T 2 =100℃ Answer
No, process is not reversible (b)
Since Therefore, the process is isothermal For an isothermal process we have
W =−R T 2 ln
V2 V1
As, for an ideal gas
P2 V 2 =R T 2
W =−P2 V 2 ln
V2 V1
4 4 W =−6 ¯¿ m3 ln 3 3∗4
W =8.788 ¯¿
m 3∗101325 N kJ ∗1 2 ¯ 1000 Nm 1.01325 ¿ m
W =878.8 kJ Answer
Problem 3.18: An ideal gas initially at 30 0C and 100 kPa undergoes the following cyclic processes in a closed system: a In mechanically reversible processes, it is first compressed adiabatically to 500 kPa then cooled at a constant pressure of 500 kPa to 30 0C and finally expanded isothermally to its original state b The cycle traverses exactly the same changes of state but each step is irreversible with an efficiency of 80% compared with the corresponding mechanically reversible process NOTE: the initial step can no longer be adiabatic Find Q W ∆ U and ∆ H for each step of the process and for the cycle Take C = (7/2) R and C = p
(5/2) R
29
V
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Given Data:
T 1 =30 0.C
T 1 =303.15 K
P1=100 kPa
Q=?
W =?
∆ U =?
∆ H=?
7 C P= R 2
5 CV = R 2
lution: (a)
P2=500 kPa 1) Adiabatic Compression from point 1 to point 2
Q12=0
Now, from first law of thermodynamics,
∆ U 12=Q12 +W 12
∆ U 12 =W 12
W 12=∆U 12=CV ∆ T 12
5 W 12=∆U 12= R ( T 2−T 1 ) → ( 1 ) 2
For ‘T2’ We know that
T 2 P2 = T 1 P1
( )
γ −1 γ
T 2 =T 1
P2 P1
( )
γ −1 γ
T 2 =303.15 K
500 100
( )
1.4−1 1.4
T 2 =480.13 K
Put in (1)
5 J kJ kJ W 12=∆U 12= ∗8.314 ( 480.13−303.15 ) K∗1 W 12=∆ U 12=3.679 2 mol∗K 1000 J mol Also, we have
∆ H 12=C P ( T 2−T 1 )
7 J kJ ∆ H 12= ∗8.314 ( 480.13−303.15 ) K∗1 2 mol∗K 1000 J
2) Cooling at constant pressure from point 2 to point 3 Therefore at constant pressure we have,
Q23=∆ H 23=C P ∆T 23
30
7 Q23=∆ H 23= R ( T 3−T 2 ) 2
∆ H 12=5.15
kJ mol
So
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Here
T 3 =303.15 K
7 J kJ kJ Q23=∆ H 23= ∗8.314 ( 303.15−480.13 ) K∗1 Q =∆ H 23=−5.15 2 mol∗K 1000 J 23 mol Also, we have
∆ U 23 =C V ( T 3−T 2) 5 J kJ ∆ U 23 = ∗8.314 ( 303.15−480.13 ) K∗1 2 mol∗K 1000 J ∆ U 23=−3.679
kJ mol
Now, from first law of thermodynamics,
∆ U 23=Q23 +W 23
W 23=∆ U 23−Q23
W 23=−3.679+5.15
W 23=1.471
3) Isothermal expansion from point 3 to point 1 Since for an isothermal process temperature remains constant Therefore,
∆ U 31=∆ H 31=0 Here
P3=P2=500 kPa
For an Isothermal process we have
500 ∗1 kJ P3 J 100 W 31=−R T 3 ln W 31=−8.314 ∗303.15 K∗ln P1 mol∗K 1000 J W 31=−4.056
31
According to first law of thermodynamics
kJ mol
kJ mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
∆ U 31 =Q31 +W 31 0=Q31+W 31
Q31=−W 31
Q31=4.056
kJ mol
For the complete cycle,
Q=Q12 +Q23+ Q31
Q=0−5.15+ 4.056
W =W 12+W 23+W 31
∆ U =∆ U 12 +∆ U 23 +∆ U 31
kJ Answer mol
W =3.679+ 1.471−4.056
W =1.094
∆ H=∆ H 12+ ∆ H 23+ ∆ H 31
Q=−1.094
kJ Answer mol
∆ H=5.15−5.15+0
∆ H=0
kJ Answer mol
∆ U =3.679−3.679+0
∆ U =0
kJ Answer mol
(b)
If each step that is 80% accomplishes the same change of state then values of
∆U
in part (a) but values of Q & W will change. 1. Adiabatic Compression from point 1 to point 2
W 12=
W 12 0.8
W 12=
3.679 0.8
W 12=4.598
kJ mol
According to first law of thermodynamics
∆ U 12 =Q12 +W 12 3.679
kJ kJ =Q12+ 4.598 mol mol
Q12=3.679
kJ kJ −4.598 mol mol
2. Cooling at constant pressure from point 2 to point 3 32
Q12=−0.92
kJ mol
&
∆H
will remain same as
August 20, 2013
PROBLEMS
ZAID YAHYA
W 23=
W 23 0.8
W 23=
1.471 0.8
11-CH-74
W 23=1.839
kJ mol
According to first law of thermodynamics
∆ U 23=Q23 +W 23
−3.679
kJ kJ =Q23 +1.839 mol mol
Q23=−3.679
kJ kJ −1.839 mol mol
kJ ∗0.8 mol
W 31=3.245
Q23=−5.518
kJ mol
3. Isothermal expansion from point 3 to point 1 Since initial step can no longer be adiabatic , therefore
W 31=W 31∗0.8
W 31=−4.056
kJ mol
According to first law of thermodynamics
∆ U 31 =Q31 +W 31
Q31=−W 31+ 0
Q31=3.245
kJ mol
For the complete cycle,
Q=Q12 +Q 23+Q31
W =W 12+W 23+W 31
Q=−0.92−5.518+ 3.245
W =4.598+1.839−3.245
W =3.192
Q=−3.193
kJ Answer mol
kJ Answer mol
Problem 3.19: One cubic meter of an ideal gas at 600 K and 1,000 kPa expands to five times its initial volume as follows: a) By a mechanically reversible, isothermal process b) By a mechanically reversible adiabatic process c) By adiabatic irreversible process in which expansion is against a restraining pressure of 100 kPa For each case calculate the final temperature, pressure and the work done by the gas, Cp=21 J mol-1K-1. Given Data:
33
August 20, 2013
V 1=1 m3
PROBLEMS
T 1 =600 K
ZAID YAHYA
P1=1000 kPa
V 2=5 V 1
V 2=5 m3
C P=21
11-CH-74
J mol K
CV =?
T 2 =?
W =?
Solution:
We know that,
C P−C V =R
CV =C P −R
CV =( 21−8.314 )
J mol∗K
CV =12.686
J mol∗K
As
γ=
CP CV
γ =1.6554
(a) Since, for an isothermal process Temperature remains constant, therefore
T 2 =T 1=600 K Answer
For an ideal gas we have
P1 V 1 P 2 V 2 = T1 T2
P1 V 1 ∗T 2 T1 P 2= V2
3
1000 kPa∗1 m ∗600 K 600 K P 2= 3 5m
We know that, for an isothermal process
W =−R T 1 ln Since
P1 V 1=R T 1 Therefore,
34
V2 V1
P2=200 kPa Answer
P2=?
August 20, 2013
PROBLEMS
ZAID YAHYA
5 ∗N 1 ∗J Pa∗m2 3 W =−1000 kPa∗1 m ln Nm
V W =−P1 V 1 ln 2 V1
11-CH-74
W =−1609.43 kJ Answer
(b)
We know that, for an adiabatic process γ
P1 V 1 =P2 V 2
V P2=P1 1 V2
1 5
1.6554
()
P2=1000 kPa∗
P2=69.65 kPa Answer
For an ideal gas we have
P1 V 1 P2 V 2 = T1 T2
γ
( )
γ
P V T 2 = 2 2 ∗T 1 P1 V 1
69.65 kPa∗5 m3 T2= ∗600 K 1000 kPa∗1 m3
T 2 =208.95 K Answer
For an adiabatic process work done is
P V −P1 V 1 W= 2 2 γ −1
N ∗J ( 69.65∗5−1000∗1 ) kPa∗m Pa∗m 2 W= 1.6554−1 Nm 3
W =−994.43 kJ Answer
(c)
Pr=100 kPa
Since, for an adiabatic process
Q=0
According to first law of thermodynamics
∆ U =Q+W
∆ U =W
∆ U =W =−Pr dV
∆ U =W =−Pr ( V 2−V 1)
3
kPa∗m ∗N ∗J 2 Pa∗m ∆ U =W =−100 ( 5−1 ) Nm
∆ U =−400 kJ
T2=
35
n CV ∆T =−400 kJ
−400 kJ + T 1 →( 1) n CV
n CV ( T 2−T 1 )=−400 kJ
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
For an ideal gas we have, 3
P1 V 1=nR T 1
n=
P1 V 1 RT1
1000 kPa∗1 m ∗mol∗K ∗kN 8.314 J∗600 K ∗kJ kPa∗m2 n= kNm
Put in (1)
−400 kJ∗mol∗K ∗1000 J 0.2005 mol∗12.686 J T2= +600 K 1 kJ
n=0.2005 mol
T 2 =−157.26 K +600 K
T 2 =442.74 K Answer
For an ideal gas we have
P1 V 1 P2 V 2 = T1 T2
P1 V 1 ∗T 2 T1 P2= V2
3
1000 kPa∗1 m ∗442.74 K 600 K P2= 3 5m
P2=147.58 kPa Answe r
Problem 3.20: One mole of air, initially at 150 0C and 8 bars undergoes the following mechanically reversible changes. It expands isothermally to a pressure such that when it is cooled at constant volume to 50 0C its final pressure is 3 bars. Assuming air is an ideal gas for which C P = (7/2) R and CV = (5/2) R, calculate W, Q, ∆ U , and ∆ H Given Data:
Mole of air=n=1mol
0
Initial Temperature=T 1=150 .C =423.15 K
Finaltemperature=T 3=50 0.C =323.15 K
Final pressure=P 3=3 ¯¿
Initial pressure=P1=8 ¯¿ 7 C P= R 2
5 CV = R 2
Solution: Since process is reversible Two different steps are used in this case to reach final state of the air.
Step 12: 36
For step 12 temperatures is constant,
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
T 1 =T 2
Therefore
∆ U 12=∆ H 12=0 For an isothermal process we have
W 12=R T 1 ln
V1 V2
As
V 2=V 3
W 12=R T 1 ln
V1 →(1) V3
We know that
P1 V 1 P 3 V 3 = T1 T3
V 1 P3 ¿T 1 = V 3 T 3∗P1
8.314 J∗423.15 K ∗1 kJ mol∗K 3∗423.15 W 12= ∗ln 1000 J 8∗323.15
P ¿T W 12=R T 1 ln 1 3 T 1∗P3 W 12=−2.502
kJ mol
According to first law of thermodynamics
∆ U 12=Q12 +W 12
0=Q12+W 12
Q12=−W 12
Q12=2.502
kJ mol
Step 23: For step 23 volume is constant, Therefore,
W 23=0
According to first law of thermodynamics
∆ U 23=Q23 +W 23
∆ U 23=Q23 +0
Q23=∆ U 23
Q23=∆ U 23=CV ∆ T
5 Q23=∆ U 23= R ( 323.15−423.15 ) K 2
37
Q23=∆ U 23=CV ( T 3−T 2 )
August 20, 2013
PROBLEMS
ZAID YAHYA
❑❑ ¿❑ ❑
11-CH-74
¿❑ ❑
¿❑❑ K ❑❑
()
¿ 8.314 ❑ ❑
¿❑❑
¿−2.0785 ❑ ❑
W e know that
∆ H 23=C P ∆ T
∆ H 23=C P ( T 3−T 2 )
J ∗1 kJ 7 mol∗K ∆ H 23= ∗8.314 ( 423.15−323.15 ) K 2 1000 J
∆ H 23=2.91
kJ mol
For the complete cycle,
Work=W =W 12 +W 23
Q=Q 12 +Q23
W = (−2.502+0 )
Q=( 2.502−2.0785 )
∆ U =∆ U 12 +∆ U 23
∆ H=∆ H 12+ ∆ H 23
kJ mol
kJ mol
W =−2.502
Q=0.424
kJ Answe r mol
kJ Answer mol
∆ U =( 0−2.0785 )
kJ mol
∆ U =−2.0785
∆ H= ( 0−2.91 )
kJ mol
∆ H=−2.91
kJ Answe r mol
kJ Answe r mol
Problem 3.21: An ideal gas flows through a horizontal tube at steady state. No heat is added and no shaft work is done. The cross-sectional area of the tube changes with length, and this causes the velocity to change. Derive an equation relating the temperature to the velocity of the gas. If nitrogen at 150 0C flows past one section of the tube with a velocity of 2.5 m/s, what is the temperature at another section where its velocity is 50 m/s? Let CP = (7/2) R Given Data:
38
August 20, 2013
PROBLEMS
ZAID YAHYA 0
Velocity=u 1=2.5
Temperature=T 1=150 .C =423.15 K
m sec
Molecualr weight of Nitrogen=28
11-CH-74
T 2 =?
u2=50
m sec
7 C P= R 2
g mol
Solution:
Applying energy balance for steady state flow process
∆ H+
∆ u2 + g ∆ z=Q+W S 2
Since
∆ z=W S=Q=0 Therefore, 2
∆u ∆ H+ =0 2
−∆u CP ∆ T = 2
2
−u22−u12 T2= + T1 2C P
−u22−u12 C P ( T 2 −T 1 )= 2
−( 50 2−2.52 )∗2∗m2∗mol∗K ∗28 g Nitrogen 2∗7∗8.314 J∗sec 2 ∗J 1 mol Nitrogen ∗N∗sec 2 N∗m ∗1 kg kg∗m T2= + 423.15 K 1000 g T 2 =421.95 K
0
T 2 =( 421.95−273.15 ) .C
0
T 2 =148.8 .C
T 2 =−1.199 K + 423.15 K
Answe r
Problem 3.22: One mole of an ideal gas, initially at 30 0C and 1 bar, is changed to 130 0C and 10 bars by three different mechanically reversible processes: a) The gas is first heated at constant volume until its temperature is 130 0C; then it is compressed isothermally until its pressure is 10 bar b) The gas is first heated at constant pressure until its temperature is 130 0C; then it is compressed isothermally to 10 bar c) The gas is first compressed isothermally to 10 bar; then it is heated at constant pressure to 130 0C 39
August 20, 2013
PROBLEMS
Calculate Q, W,
ZAID YAHYA
∆ U ∧∆ H
11-CH-74
in each case. Take CP = (7/2) R and CV = (5/2) R. alternatively, take CP =
(5/2) R and CV = (3/2) R Given Data:
T 1 =30 0.C
T 1 =( 30+273.15 ) K T 3 =403.15 K
P1=1 ¯¿
T 1 =303.15 K P3=10 ¯¿
Q=?
W =?
T 2 =130 0.C ∆ U =?
T 3 =( 130+273.15 ) K ∆ H=?
Solution: 7 C P= R 2
5 CV = R 2
Each part consist of two steps, 12 & 23 For the overall processes
∆ U =∆ U 12=∆U 23=CV ∆T
5 ∆ U =∆ U 12=∆U 23= R ( T 3−T 1 ) 2
5 J K∗1 kJ ∆ U =∆ U 12=∆U 23= ∗8.314 ( 403.15−303.15 ) 2 mol∗K 1000 J ∆ U =∆ U 12=∆U 23=2.079
kJ →(a) Answe r mol
Now
∆ H=∆ H 12=∆ H 23=C P ∆ T 7 ∆ H=∆ H 12=∆ H 23= R ( T 2−T 1) 2 7 J kJ ∆ H=∆ H 12=∆ H 23= ∗8.314 ( 403.15−303.15 ) K∗1 2 mol∗K 1000 J ∆ H=∆ H 12=∆ H 23=2.91
40
kJ → ( b ) Answe r mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
(a)
Step 12: For step “12” volume is constant Therefore
W 12=0 Here
T 2 =T 3
According to first law of thermodynamics
∆ U 12=Q12 +W 12
∆ U 12=Q12
Q12=∆ U 12=C V ∆ T
Q12=∆ U 12=2.079
kJ [¿ ( a ) ] mol
Also we have
∆ H 12=2.91
kJ [ ¿( b)] mol
Step 23: Since for step “23” process is isothermal Therefore
∆ U 23 =∆ H 23=0 Here
T 2 =T 3 Now, intermediate pressure can be calculated as
P1 P2 = T1 T 2
P P2= 1∗T 2 T1
¯¿ ∗403.15 K 303.15 K P2=¿
P2=1.329 b ar
For an isothermal process we have
W 23=R T 2 ln 41
1
P3 P2
W 23=8.314
J K∗1 kJ 10 ∗403.15 ∗ln mol∗K 1000 J 1.329
August 20, 2013
PROBLEMS
ZAID YAHYA
W 23=6.764
11-CH-74
kJ mol
According to first law of thermodynamics
∆ U 23=Q23 +W 23
0=Q23+W 23
Q23=−W 23
Q23=−6.764
kJ mol
For the complete cycle,
Work=W =W 12 +W 23
Q=Q12 +Q23
W = ( 0+6.764 )
Q=( 2.079−6.764 )
∆ U =∆ U 12 +∆ U 23
kJ mol
kJ mol
W =6.764
Q=−4.685
kJ Answe r mol
∆ U =( 2.079+0 )
kJ mol
∆ U =2.079
∆ H= ( 2.91+ 0 )
kJ mol
∆ H=2.91
∆ H=∆ H 12+ ∆ H 23
kJ Answe r mol
kJ Answe r mol
kJ Answe r mol
(b)
Step 12: For step “12” volume is constant Therefore, at constant pressure we have
Q12 ¿ ∆ H 12=2.91
kJ mol
[ ¿(b)]
Also,
∆ U 12 =2.079
[ ¿(a)]
According to first law of thermodynamics
∆ U 12=Q12 +W 12
42
kJ mol
W 12=∆U 12−Q12
W 12=( 2.079−2.91 )
kJ mol
W 12=−0.831
kJ mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Step 23: Since for step “23” process is isothermal ( T = Constant) Therefore
∆ U 23 =∆ H 23=0 Here
T 2 =T 3∧P 1=P2
For an isothermal process we have
W 23=R T 2 ln
P3 P2
W 23=8.314
J K∗1 kJ 10 ∗403.15 ∗ln mol∗K 1000 J 1
W 23=7.718
kJ mol
According to first law of thermodynamics
∆ U 23 =Q23 +W 23
0=Q23+W 23
Q23=−W 23
Q23=−7.718
kJ mol
For the complete cycle,
Work=W =W 12 +W 23
Q=Q12 +Q23
W = (−0.831+7.718 )
Q=( 2.91−7.718 )
∆ U =∆ U 12 +∆ U 23
∆ H=∆ H 12+ ∆ H 23
kJ mol
kJ mol
Q=−4.808
kJ mol
∆ U =2.079
∆ H= ( 2.91+ 0 )
kJ mol
∆ H=2.91
Since for step “12” process is isothermal ( T = Constant) Therefore
∆ U 12=∆ H 12=0
43
kJ Answer mol
kJ Answe r mol
∆ U =( 2.079+0 )
(c)
Here
W =6.887
kJ Answe r mol
kJ Answe r mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
P2=P3
For an isothermal process we have
W 12=R T 1 ln
P2 P1
W 12=8.314
W 12=5.8034
J K∗1 kJ 10 ∗303.15 ∗ln mol∗K 1000 J 1 kJ mol
According to first law of thermodynamics
∆ U 12=Q12 +W 12
0=Q12+W 12
Q12=−W 12
Q12=−5.8034
kJ mol
Step 23: For step “23” volume is constant Therefore, at constant pressure we have
Q23=∆ H 23=2.91
kJ [¿ (b)] mol
Here
T 2 =T 3 Now
∆ U 23=2.079
kJ [ ¿(a)] mol
According to first law of thermodynamics
∆ U 23=Q23 +W 23
W 23=∆ U 23−Q23
W 23=( 2.079−2.91 )
kJ mol
W 23=−0.831
For the complete cycle,
Work=W =W 12 +W 23
44
W = (5.8034−0.831 )
kJ mol
W =4.972
kJ Answer mol
kJ mol
August 20, 2013
PROBLEMS
ZAID YAHYA
Q=Q 12 +Q23
Q=(−5.8034+2.91 )
∆ U =∆ U 12 +∆ U 23
∆ H=∆ H 12+ ∆ H 23
kJ mol
Q=−2.894
11-CH-74
kJ Answe r mol
∆ U =( 0+2.079 )
kJ mol
∆ U =2.079
∆ H= ( 0+2.91 )
kJ mol
∆ H=2.91
kJ Answe r mol
kJ Answe r mol
Solution: 5 C P= R 2
3 CV = R 2
Each part consist of two steps, 12 & 23 For the overall processes
∆ U =∆ U 12=∆U 23=CV ∆T
3 ∆ U =∆ U 12=∆U 23= R ( T 3 −T 1 ) 2
3 J K∗1 kJ ∆ U =∆ U 12=∆U 23= ∗8.314 ( 403.15−303.15 ) 2 mol∗K 1000 J ∆ U =∆ U 12=∆U 23=1.247
kJ →(a) Answe r mol
Now
∆ H=∆ H 12=∆ H 23=C P ∆ T 5 ∆ H=∆ H 12=∆ H 23= R ( T 2−T 1 ) 2 5 J kJ ∆ H=∆ H 12=∆ H 23= ∗8.314 ( 403.15−303.15 ) K∗1 2 mol∗K 1000 J ∆ H=∆ H 12=∆ H 23=2.079
45
kJ → ( b ) Answer mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
(a)
Step 12: For step “12” volume is constant Therefore
W 12=0 Here
T 2 =T 3
According to first law of thermodynamics
∆ U 12 =Q12 +W 12
∆ U 12 =Q12
Q12=∆ U 12=C V ∆ T
Q12=∆ U 12=1.247
Also we have
∆ H 12=2.079
kJ [ ¿( b)] mol
Step 23: Since for step “23” process is isothermal Therefore
∆ U 23 =∆ H 23=0 Here
T 2 =T 3 Now, intermediate pressure can be calculated as
P1 P2 = T1 T 2
46
P P2= 1∗T 2 T1
For an isothermal process we have
1
¯¿ ∗403.15 K 303.15 K P2=¿
P2=1.329 b ar
kJ [ ¿( a) ] mol
August 20, 2013
PROBLEMS
ZAID YAHYA
W 23=R T 2 ln
P3 P2
W 23=8.314
J K∗1 kJ 10 ∗403.15 ∗ln mol∗K 1000 J 1.329
W 23=6.764
11-CH-74
kJ mol
According to first law of thermodynamics
∆ U 23=Q23 +W 23
0=Q23+W 23
Q23=−W 23
Q23=−6.764
kJ mol
For the complete cycle,
Work=W =W 12 +W 23
Q=Q 12 +Q23
W = ( 0+6.764 )
Q=( 1.247−6.764 )
kJ mol
kJ mol
W =6.764
Q=−5.516
kJ Answe r mol
kJ Answe r mol
∆ U =∆ U 12 +∆ U 23
∆ U =( 1.247+0 )
kJ mol
∆ U =1.247
kJ Answer mol
∆ H=∆ H 12+ ∆ H 23
∆ H= ( 2.079+ 0 )
kJ mol
∆ H=2.079
kJ Answe r mol
(b)
Step 12: For step “12” volume is constant Therefore, at constant pressure we have
Q12 ¿ ∆ H 12=2.079
kJ mol
[ ¿(b)]
Also,
∆ U 12 =1.247
47
kJ mol
According to first law of thermodynamics
[ ¿(a)]
August 20, 2013
PROBLEMS
ZAID YAHYA
∆ U 12 =Q12 +W 12
W 12=∆U 12−Q12
11-CH-74
W 12=( 1.247−2.079 )
kJ mol
W 12=−0.832
Step 23: Since for step “23” process is isothermal ( T = Constant) Therefore
∆ U 23 =∆ H 23=0 Here
T 2 =T 3∧P 1=P2
For an isothermal process we have
W 23=R T 2 ln
P3 P2
W 23=8.314
J K∗1 kJ 10 ∗403.15 ∗ln mol∗K 1000 J 1
W 23=7.718
kJ mol
According to first law of thermodynamics
∆ U 23 =Q23 +W 23
0=Q23+W 23
Q23=−W 23
Q23=−7.718
kJ mol
For the complete cycle,
Work=W =W 12 +W 23
Q=Q12 +Q23
(c)
Step 12: 48
W = (−0.832+7.718 )
Q=( 2.079−7.718 )
kJ mol
kJ mol
W =6.886
Q=−5.639
kJ Answer mol
kJ Answer mol
∆ U =∆ U 12 +∆ U 23
∆ U =( 1.247+0 )
kJ mol
∆ U =1.247
kJ Answer mol
∆ H=∆ H 12+ ∆ H 23
∆ H= ( 2.079+ 0 )
kJ mol
∆ H=2.079
kJ Answe r mol
kJ mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Since for step “12” process is isothermal ( T = Constant) Therefore
∆ U 12=∆ H 12=0 Here
P2=P3
For an isothermal process we have
W 12=R T 1 ln
P2 P1
W 12=8.314
W 12=5.8034
J K∗1 kJ 10 ∗303.15 ∗ln mol∗K 1000 J 1 kJ mol
According to first law of thermodynamics
∆ U 12=Q12 +W 12
0=Q12+W 12
Q12=−W 12
Q12=−5.8034
kJ mol
Step 23: For step “23” volume is constant Therefore, at constant pressure we have
Q23=∆ H 23=2.079
kJ [ ¿(b)] mol
Here
T 2 =T 3 Now
∆ U 23=1.247
According to first law of thermodynamics
∆ U 23=Q23 +W 23 For the complete cycle, 49
kJ [ ¿(a)] mol
W 23=∆ U 23−Q23
W 23=( 1.247−2.079 )
kJ mol
W 23=−0.832
kJ mol
August 20, 2013
PROBLEMS
ZAID YAHYA
Work=W =W 12 +W 23
Q=Q 12 +Q23
W = (5.8034−0.832 )
Q=(−5.8034+2.079 )
kJ mol
11-CH-74
W =4.9714
kJ mol
Q=−3.724
kJ Answe r mol
kJ Answe r mol
∆ U =∆ U 12 +∆ U 23
∆ U =( 0+1.247 )
kJ mol
∆ U =1.247
kJ Answer mol
∆ H=∆ H 12+ ∆ H 23
∆ H= ( 0+2.079 )
kJ mol
∆ H=2.079
kJ Answe r mol
Problem 3.23: One mole of an ideal gas, initially at 30
℃
and 1 bars, undergoes the following mechanically
reversible changes. It is compressed isothermally to point such that when it is heated at constant volume to 120 ℃ its final pressure is 12 bars. Calculate Q, W, ∆ U ∧∆ H for the process. Take C (7/2) R and P=
CV = (5/2) R. Given Data:
T 1 =30℃ T 3 =393.15 K
T 1 =( 30+273.15 ) K P3=12 ¯¿
Q=?
T 1 =303.15 K W =?
P1=1 ¯¿
∆ U =?
∆ H=?
Solution:
The process consist of two steps, 12 & 23
Step 12: Since for step “12” process is isothermal ( T = Constant) Therefore
∆ U 12=∆ H 12=0 Now, intermediate pressure can be calculated as 50
T 3 =120℃ 7 C P= R 2
T 3 =( 120+273.15 ) K 5 CV = R 2
August 20, 2013
PROBLEMS
P2 T2
ZAID YAHYA
P ¿ 3 T3
P P2= 3 ∗T 2 T3
12
¯¿ ∗303.15 K 393.15 K P2=¿
P2=9.25 b ar
For an isothermal process we have
W 12=R T 1 ln
P2 P1
W 12=8.314
J K∗1 kJ 9.25 ∗303.15 .15 ∗ln mol∗K 1000 J 1
W 12=5.607
11-CH-74
kJ mol
According to first law of thermodynamics
∆ U 12=Q12 +W 12
0=Q12+W 12
Q12=−W 12
Q12=−5.607
kJ mol
Step 23: Since for step “23” volume is constant Therefore
W 23=0
According to first law of thermodynamics
∆ U 23 =Q23 +W 23
∆ U 23=Q23
Q23=∆ U 23=CV ∆ T
5 Q23=∆ U 23= R ( T 3−T 1 ) 2
5 J K∗1 kJ kJ Q23=∆ U 23= ∗8.314 ( 393.15−303.15 ) Q23=∆ U 23=1.871 2 mol∗K 1000 J mol Now
∆ H 23=C P ∆ T 7 ∆ H 23= R ( T 2−T 1 ) 2
51
7 J kJ ∆ H 23= ∗8.314 (393.15−303.15 ) K∗1 2 mol∗K 1000 J
∆ H 23=2.619
kJ mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
For the complete cycle,
Work=W =W 12 +W 23
Q=Q 12 +Q23
W = (5.607 +0 )
Q=(−5.607+1.871 )
kJ mol
kJ mol
W =5.607
Q=−3.736
kJ Answe r mol
kJ Answe r mol
∆ U =∆ U 12 +∆ U 23
∆ U =( 0+1.871 )
kJ mol
∆ U =1.871
kJ Answe r mol
∆ H=∆ H 12+ ∆ H 23
∆ H= ( 0+2.691 )
kJ mol
∆ H=2.691
kJ Answe r mol
Problem 3.24: A process consists of two steps: (1) One mole of air at T = 800 K and P = 4 bars are cooled at constant volume to T = 350 K. (2) The air is then heated air constant pressure until its temperature reaches 800 K. If this two step process is replaced by a single isothermal expansion of the air from 800 K and 4 bar to some final pressure P, what is the value of P that makes the work of two step processes the same? Assume mechanical reversibility and treat air as an ideal gas with CP = (7/2) R and CV = (5/2) T. Given Data:
T 1 =800 K
P1=4 ¯¿
T 2 =350 K
P=?
Solution: For the first step volume is constant Therefore,
W 12=0 For the work done is
W =W 23=−P 2 ∆V →(1)
For one mole of an ideal gas we have,
P ∆ V =R ∆ T 52
P2 ∆ V =R ∆ T
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Put in (1)
W =−R ( T 3−T 2 )
W =−R ∆ T Since
T 3 =T 1 Therefore
W =−R ( T 1−T 2) →(2)
For an isothermal process we have
W =R T 1 ln
P → (3) P1
Compare (2) and (3)
P −R ( T 1−T 2 )=R T 1 ln P1
T 2−T 1 P =ln T1 P1
P T 2 −T 1=T 1 ln P1 4 ¯¿ 0.5698=P
P 4 ¯¿ ( 350−800 ) K =ln ¿ 800 K
4 ¯¿ P e−0.5625= ¿
¯ P=2.279 Answer
Problem 3.25: A scheme for finding the internal volume
V tB
of the gas cylinder consists of the following steps. The
cylinder is filled with a gas to low pressure P 1, and connected through a small line and valve to an t
evacuated reference tank of known volume V A . The valve is opened, and the gas flows through the line into the reference tank. After the system returns to its initial temperature, a sensitive pressure transducer provides a valve for the pressure change from the following data: t 3 a) V A =256 cm b)
∆ P/ P1=−0.0639
Given Data: 53
∆P
in the cylinder. Determine the cylinder volume
t
VB
August 20, 2013
PROBLEMS
V tB =?
ZAID YAHYA
V tA =256 cm3
11-CH-74
∆P =−0.0639 P1
Solution: ∆P =−0.0639 P1
P2 −P 1 =−0.0639 P1
P2 −1=−0.0639 P1
P2 =−0.0639+1 P1
P2 =0.9361 →(1) P1
Assume that gas is ideal & P2 is the pressure of the tank When gas flows through the line into the tank then tank’s total volume becomes
t
t
V A +V B
Now, by applying condition for an ideal gas t B
t A
P1 V =P2 ( V +V
t B
)
P2 Vt = t B t P1 V A +V B
Put in (1)
V tB =0.9361 V tA +V tB
V tB =0.9361 ( V tA +V tB )
V tB ( 1−0.9361 ) =0.9361V tA
V tB =0.9361V tA +0.9361V tB
0.0639 V tB =256 cm 3∗0.9361
t
V B=
V tB −0.9361V tB=0.9361V tA
239.6461 3 cm 0.0639
V tB =3750.26 cm 3 Answe r
Problem 3.26: A closed, non-conducting, horizontal cylinder is fitted with non-conducting, frictionless, floating piston which divides the cylinder in two Sections A & B. The two sections contains equal masses of air, initially at the same conditions, T1 = 300 K and P1 = 1 atm. An electrical heating element in section A is activated, and the air temperature slowly increases: TA in section A because of heat transfer, and T B in section B because of adiabatic compression by slowly moving piston. Treat air as an ideal gas with C P = (7/2) R and let nA be the number of moles of air in section A. For the process as described, evaluate one of the following sets of quantities: a) TA, TB, and Q/ nA, if P (final) = 1.25 atm b) TB, Q/ nA, and P (final), if TA = 425 K c) TA, Q/nA, and P (final), if TB = 325 K d) TA, TB, and P (final), if Q/nA = 3 kJ mol-1. Given Data:
54
August 20, 2013
T 1 =300 K
PROBLEMS
P1=1 atm
ZAID YAHYA
11-CH-74
7 C P= R 2
Solution:
According to ideal gas equation,
PV =nRT Applying ideal gas equation for initial conditions On section “A”
P1 V A =n A R T 1
V A=
nART1 P1
On section “B”
P1 V B=n B RT 1 Since
n A =n B Therefore,
P1 V B=n A R T 1
V B=
n A RT 1 P1
Total initial volume can be given as
V i=V A + V B
V i=
nA R T1 nA R T1 + P1 P1
V i=2.
n A RT 1 P1
Let P2 be the final pressure & TA & TB are the final temperatures of section A & section B respectively Applying ideal gas equation for final conditions On section “A”
P2 V A =n A R T A V A=
nART A P2
On section “B”
P2 V B=n A R T B Total Final volume can be given as 55
V B=
n A RT B P2
August 20, 2013
V f =V A +V B
PROBLEMS
Vf=
ZAID YAHYA
nA R T A nA R T B + P2 P2
Vf=
11-CH-74
nA R (T A+ T B) P2
Since the total volume is constant, therefore
V i=V f
2.
n A R T 1 n A R ( T A +T B ) 2. T 1 ( T A +T B ) = = →(1) P1 P2 P1 P2
(a)
P2=1.25 atm
Since the process occurring in section B is reversible adiabatic compression Therefore, for an adiabatic compression we have
T 1 ( P1 )
1−γ γ
=T B ( P2 )
T B=T 1
1−γ γ
P2 P1
( )
T B=
T 1 ( P1 )
( P 2) γ−1 γ
1−γ γ
1− γ γ
→(2)
We know that,
C P−C V =R
CV =C P −R
7 CV = R−R 2
CV =
7 R−2 R 2
5 CV = R 2
As
γ=
CP CV
γ=
7∗R∗2 2∗5∗R
γ =1.4
Put in (2)
T B=300 K
1.25 1
( )
1.4 −1 1.4
T B=300 K∗1.0658
T B=319.74 K Answe r
56
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Put in (1)
2∗300 K ( T A +319.74 K ) = 1 atm 1.25 atm 600 K∗1.25=T A +319.74 K
T A =750 K−319.74 K
T A =430.26 K Answe r
According to first law of thermodynamics
∆ U =Q+W Since volume is constant, therefore
∆ U =Q→( a) For section A & B
∆ U =∆ U A +∆ U B Put in (a)
Q=∆U A + ∆U B
Q=n A CV ∆ T +n A C V ∆ T
Q=n A CV [ T A +T B−2T 1 ]
Q=n A CV ( T A−T 1 ) +n A C V ( T B −T 1 )
Q =C V [ T A +T B −2 T 1 ] →(3) nA
Q 5 J K∗1 kJ = ∗8.314 ∗150.02 nA 2 mol∗K 1000 J
Q 5 = R ( 430.26+ 319.74−2∗300 ) K nA 2 Q kJ =3.118 Answe r nA mol
(b)
T A =425 K From equation (1)
2. T 1 ( T A +T B ) = P1 P2 Put in (2)
57
Q=n A CV [ T A−T 1 +T B−T 1 ]
P2 ( T A +T B ) = P1 2.T 1
August 20, 2013
PROBLEMS
ZAID YAHYA
T B=T 1
Assume
)
1.4−1 1.4
T B=300 K∗( 1.0634 ) Since
)
γ −1 γ
T B=319 K
425+ 319 T B=300 K 2∗300
(
(
T A +T B 2. T 1
11-CH-74
T B=319.02 K
319 ≈ 319.02 , therefore
T B=319.02 K Answe r Put in (1)
2∗300 K ( 425+319.02 ) K = 1 atm P2
P2=
744.02 atm 600
P2=1.24 atm Answe r
From equation (3)
Q =C V [ T A +T B −2 T 1 ] nA Q 5 = R ( 425+319.02−2∗300 ) K nA 2 Q 5 J K∗1 kJ Q kJ = ∗8.314 ∗144.02 =2.993 Answer nA 2 mol∗K 1000 J n A mol (c)
T B=325 K Put in (2)
58
August 20, 2013
T B=T 1
PROBLEMS
P2 P1
( )
γ−1 γ
ZAID YAHYA
P2 325 K=300 K 1 atm
( )
γ −1 γ
P2 325 = 300 1 atm
( )
γ −1 γ
11-CH-74
325 300
( )
γ γ −1
=
P2 1 atm
325 300
( )
P2=
1.4 1.4−1
P2=1.323 atm Answe r Put in (1)
2. T 1 ( T A +T B ) = P1 P2
2∗300 K T A +325 K = 1 atm 1.323 atm
T A +325 K =600 K∗1.323
T A =793.9 K−325 K
T A =468.9 K Answe r From equation (3)
Q =C V [ T A +T B −2 T 1 ] nA Q 5 = R ( 468.9+325−2∗300 ) K nA 2 Q 5 J K∗1 kJ Q kJ = ∗8.314 ∗193.9 =4.0302 Answe r nA 2 mol∗K 1000 J n A mol (d)
Q kJ =3 nA mol From equation (1)
2. T 1 ( T A +T B ) = P1 P2
T A +T B=
2.T 1∗P2 → (b ) P1
From equation (3)
Q =C V [ T A +T B −2 T 1 ] nA Comparing (b) and (c) 59
T A +T B−2 T 1 =
Q n A∗C V
T A +T B=
Q + 2T 1 →(c ) n A∗C V
atm
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
2. T 1∗P2 Q = +2 T 1 P1 n A∗CV
P 2=
P1 Q +2 T 1 2.T 1 n A∗C V
[
]
P 2=
[
1 atm 2∗3 kJ +2∗300 K 2∗300 K 5 R∗mol
P 2=
]
[
6 kJ∗mol∗K ∗1000 J 1 atm 5∗mol∗8.314 J P 2= +600 K 600 K 1 kJ
]
1 atm [ 144.335+ 600 ] K P2=1.2406 atm Answe r 600 K
Put in (2)
T B=T 1
P2 P1
( )
γ−1 γ
T B=300 K
(
1.2406 1
)
1.4 −1 1.4
T B=300 K∗1.0635
T B=319.06 K Answer Put in (1)
2. T 1 ( T A +T B ) = P1 P2 2∗300 K ( T A + 319.06 K ) = 1 atm 1.2406 atm 600 K∗1.2406=T A +319.06 K
T A =744.36 K−319.06 K
T A =425.3 K Answe r
Problem 3.27: One mole of an ideal gas with constant heat capacities undergoes an arbitrary mechanically reversible process. Show that: 1 ∆U= ∆ ( PV ) γ−1 60
August 20, 2013
PROBLEMS
ZAID YAHYA
Given Data:
Number of moles=n=1
Solution:
We know that
∆ U =nCV ∆ T
∆ U =1.C V ∆ T
∆ U =CV ( T 2−T 1 ) →(1)
For an ideal gas we have,
C P−C V =R
C P CV R − = C V CV C V
CP R −1= CV CV
Since
γ=
CP CV
Therefore,
γ −1=
R CV
CV =
R γ −1
Put in (1)
∆U=
R ( T −T ) γ−1 2 1
∆U=
For one mole of an ideal gas we have
P1 V 1=R T 1 →( a) Put (a) & (b) in (2)
∆U=
1 ( P V −P1 V 1 ) γ −1 2 2
Problem 3.28: 61
1 ( R T 2−R T 1 ) →( 2) γ−1
∆U=
1 ∆ ( PV ) Proved γ−1
P2 V 2 =R T 2 →( b)
11-CH-74
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Derive an equation for the work of a mechanically reversible, isothermal compression of 1 mole of a gas from an initial pressure p1 to a final pressure p2 when the equation of state is the virial expansion truncated to: Z =1+ B ' P How does the result compare with the corresponding equation for an ideal gas?
Solution:
For a mechanically reversible process we have, V2
W =−∫ PdV →(1) V1
Given that
Z =1+ B ' P Also
Z=
PV RT
Therefore,
PV ' =1+ B P RT
V=
RT ( 1+ B' P ) P
V =RT
( P1 + B' )
Differentiate both sides w.r.t to pressure
dV −1 =RT 2 +0 dP P
(
)
dV =
−RT dP P2
Put in (1) V2
W =−∫ PdV V1
P2
RT W =−∫ −P 2 dP P P 1
P2
W =RT ∫ P1
W =RT ln
62
1 dP P
P2
W =RT |ln P|P
P2 Proved P1
1
W =RT ( ln P 2−ln P1 )
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Problem 3.30: For methyl chloride at 100 ℃ the second and third virial coefficients are: B=−242.5 cm3 mol−1 ; C=25 200 cm 6 mol−2 . Calculate the work of mechanically reversible, isothermal compression of 1 mol of methyl chloride 1 bar to 55 bars at 100 ℃ . Base calculations on the following forms of virial equations B C Z =1+ + 2 a) V V b)
Z =1+ B' P+C ' P2 '
B=
Where
B C−B 2 ' ∧C = RT ( RT )2
Why don’t both equations give exactly the same result? Given Data:
Temperature=T =100 ℃ 6
C=25200 cm mol
−2
T =( 100+273.15 ) K
T =373.15 K
P1=1 ¯¿
B '=
P2=55 ¯ ¿
B RT
B=−242.5 cm3 mol−1 '
C=
C−B2 ( RT )2
Solution: As
B'=
B RT
¯¿∗1 m3 100 3 cm3 −242.5 cm3∗mol∗K ∗J mol∗8.314 J∗373.15 K ∗101325 N N∗m ' B= ¿ m2∗1.01325
Now,
63
¯¿
1 B =−7.817∗10−3 ¿ '
W =?
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
¿¯2∗1 m6 1006 cm 6 [ 25200−(−242.5 )2 ] cm6∗K 2∗mol 2 ∗J 2 mol2∗8.3142 J 2∗373.152 K 2 2 2 ∗101325 N 2 2 N ∗m C' = ¿ m4∗1.013252
2
C−B C= ( RT )2 '
¿¯2 C' =−3.492∗10−5
(a)
Z =1+
B C + V V2
PV B C =1+ + 2 RT V V
P=
RT B C 1+ + 2 →(1) V V V
(
)
For a mechanically reversible process we have, V2
W =−∫ PdV →(2) V1
Put (1) in (2) V2
RT B C W =−∫ 1+ + 2 dV V V V V 1
(
)
V2
(
W =−RT ∫ 1+ V1
B C 1 + dV →(3) V V2 V
)
Again using
V 1=
RT B C 1+ + 2 → ( 4 ) P1 V1 V1
(
)
Assume that 3
V 1=30780
cm →(a) mol ¯¿∗N∗m ∗1.01325 ¯¿ m2 J ∗1003∗cm 3 101325 N RT cm3 mol∗K∗1 =31023.6 →(b) P1 mol 1 m3 RT 8.314 J∗373.15 K = ¿ P1
64
1 ¿
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Put (a) and (b) in (4)
30780
cm3 cm3 242.5 25200 =31023.6 ∗ 1− + mol mol 30780 307802
(
)
cm3 cm3 ( 30780 =31023.6 1−0.007878+ 0.000026598 ) mol mol
cm3 cm3 30780 =31023.6∗0.99215 mol mol
cm3 cm3 30780 =30780 mol mol Since
L. H . S=R . H . S Therefore 3
Initial volume=V 1=30780
cm mol
Again using
V 2=
RT B C 1+ + 2 → (5 ) P2 V2 V2
(
)
Assume that
V 2=241.33
cm3 →( c) mol ¯¿∗N∗m ∗1.01325 ¯¿ m2 J ∗100 3∗cm3 101325 N RT cm 3 mol∗K∗55 =564.067 →(d ) P2 mol 1 m3 RT 8.314 J∗373.15 K = ¿ P2
Put (c) and (d) in (4)
65
August 20, 2013
PROBLEMS
ZAID YAHYA
3
3
241.33
cm cm 242.5 25200 =564.067 ∗ 1− + mol mol 241.33 241.332
241.33
cm3 cm3 =564.067∗0.4278 mol mol
(
241.33
)
11-CH-74 3
3
cm cm ( 241.33 =564.067 1−1.0048+ 0.4327 ) mol mol
cm3 cm3 =241.33 mol mol
Since
L. H . S=R . H . S Therefore
Finalvolume=V 2=241.33
cm 3 mol
Now from equation (3) V2
W =−RT ∫ V1
(
[
B C 1 1+ + 2 dV V V V
)
V2
W =−RT |ln V|V −B
[
W =−RT ln
1
V2
|| 1 V
W =−RT
| |]
1 1 − C 2 2 V V 1
V2
[
V2
V2
V2
1
1
1
∫ V1 dV + B ∫ V12 dV +C ∫ V13 dV V V V
V1
V2 1 1 1 1 1 −B − − C − V1 V 2 V 1 2 V 22 V 12
(
[
W =−RT ( ln V 2−ln V 1 )−B
) (
(
]
1 1 1 1 1 − − C − 2 2 V2 V1 2 V2 V1
) (
)]
−8.314∗J∗373.15 K ∗1 kJ mol∗K 241.33 1 1 25200 1 1 W= ln +242.5 − − − 2 2 1000 J 30780 241.33 30780 2 241.33 30780
[
W =−3.102
)]
(
)
(
)]
kJ kJ [ −4.848+0.996−0.2163 ] W =12.62 Answer mol mol
(b)
Z =1+ B' P+C' P 2
PV =1+ B' P+C ' P2 RT
V=
Differentiate w.r.t to pressure on both sides 66
RT ( 1+ B' P+ C' P2 ) P
V =RT
( P1 + B +C ' P) '
August 20, 2013
PROBLEMS
ZAID YAHYA
dV −1 =RT 2 +0+C ' dP P
(
)
11-CH-74
( P1 +C ' ) dP
dV =−RT
2
Put in (2) P2
1 W =−∫ −PRT 2 +C ' dP P P
(
1
)
[
[
P2
P2
1
1
1 W =RT ∫ dP+C ' ∫ PdP P P P '
C W =RT |lnP|P + |P2|P
[
W =RT ln
P2 +C' ( P22−P12 ) P1
]
P2 1
2
P2 1
]
¿¯2 ¿¯2 ( 55 2−1 ) ¿ 55 3.492∗10−5 1 ln − ¿ 1 2 8.314∗J∗373.15 K ∗1 k J mol∗K W= ¿ 1000 J W =12.268
]
W=
3.102 kJ ( 3.9545 ) mol
kJ Answer mol
The answers for part (a) and (b) differ because the relations between the two sets of parameters are exact only for infinite series
Problem 3.32: Calculate Z and V for ethylene at 25 oC and 12 bars by the following equations: a) The truncated virial equation [Eq. (3.40)] with the following experimental values of virial coefficients: B=−140 cm 3 mol−1 C=7200 cm 6 mol−2 b) The truncated virial equation [Eq.(3.38)], with a value of B from the generalized Pitzer correlations [Eq. (3.63)] c) The Redlich/Kwong equation d) The Soave/Redlich/Kwong equation e) The Peng/Robinson equation. Given Data:
67
August 20, 2013
PROBLEMS
ZAID YAHYA
Temperature=T =25 ℃
11-CH-74
T =298.15 K
T =( 25+273.15 ) K
Pressure=P=12 ¯¿
Solution: (a) 3
B=−140 cm mol
6
−1
C=7200 cm mol
−2
Given equation is
Z =1+
B C + V V2
PV B C =1+ + 2 RT V V
V=
RT B C 1+ + 2 → ( 1 ) P V V
(
)
mol∗K∗12∗¯¿∗N∗m ∗1.01325 ¯¿ m2 J ∗1003∗cm 3 101325 N 1 m3 RT 8.314∗J∗298.15 K = ¿ P
RT cm3 =2065.68 V mol Put in (1) 3
cm B C V =2065.68 1+ + 2 mol V V
(
)
Assume
V =1919
cm3 mol
Therefore 3
1919
Since
68
3
cm cm 140 7200 =2065.68 1− + mol mol 1919 19192
(
)
3
1919
3
cm cm ( =2065.68 0.9290 ) mol mol
3
1919
3
cm cm =1919 mol mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
L. H . S=R . H . S Therefore
V =1919
cm3 Answer mol
We know that
Z=
PV RT
12∗¯¿ 1919∗cm3∗mol∗K ∗J 8.314∗J∗298.15∗K∗mol ∗101325 N N∗m ∗1m 3 2 ¯ 1.01325 ¿ m Z= 1003 cm3
Z =0.929 Answer
(b)
Given equation 3.38 is
Z =1+
BP →( 2) RT
We know that
Reduced temperature=T r =
T Tc
Reduced Pressure=Pr =
T =T r T c → ( a )
Put (a) and (b) in (2)
Z =1+
B Pr Pc R T r Tc
Since
^ B Pc Reduced second virial coefficient =B= R Tc Therefore
Z =1+ Also 69
^B P r →(3) Tr
P Pc
P=Pr Pc →(b)
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
O ^ B=B +ω B1
Put in (3)
Z =1+ ( B O +ω B1 )
Pr →( 4) Tr
For ethylene (From Table B.1 Appendix B)
ω=0.087 →(i)
Critical temperature=T c =282.3 K
Critical pressure=Pc =50.40 ¯ ¿
Tr=
T 298.15 K = =1.056→(ii) T c 282.3 K
50.40 ¯¿ =0.238 →(iii) ¯ 12 ¿¿ P Pr = =¿ Pc
Also we have
B o=0.083−
0.422 T r1.6
B o=0.083−
0.422 1.6 1.056
B o=−0.304 → ( iv )
B 1=0.139−
0.172 4.2 1.056
B 1=2.183∗10−3 →( v) Put (i), (ii), (iii), (iv) & (v) in (4)
Z =1+ (−0.304+0.087∗2.183∗10−3 )
0.238 1.056
Z =0.931 Answer
We know that
Z=
PV RT
V=
ZRT P
¯¿∗N∗m ∗1.01325 ¯¿ m2 J 3 3 ∗100 cm 101325 N mol∗K∗12 1m3 0.931∗8.314 J∗298.15 K V= ¿
(c) 70
The Redlich/Kwong equation is
V =1923.
cm3 Answer mol
August 20, 2013
PROBLEMS
ZAID YAHYA
Z =1+ β−qβ
11-CH-74
Z−β → ( 5) ( Z + ϵ β ) ( Z +σβ )
Where
β=Ω
Pr Tr
From table 3.1
σ =1, Ω=0.08664, ε=0,ψ=0.42748,α ( T r )=T r
−1 2
Now
β=
0.08664∗0.238 1.056
β=0.0195 →(i ' )
Also
q=
ψα ( T r ) ΩT r
−1
0.42748∗1.056 2 q= 0.08664∗1.056
q=4.547 →(i i' )
Put (i’) and (ii’) in (5)
Z =1+ 0.0195−4.547∗0.0195
Z−β ( Z + ϵ β ) ( Z +σβ )
Assume
Z =0.928
0.928=1.0195−0.08866
0.928−0.0195 0.928 ( 0.928+ 0.0195 )
0.928=1.0195−0.08866∗1.033
Since
L. H . S=R . H . S Therefore,
Z =0.928 Answer 71
We know that
0.928=0.928
August 20, 2013
Z=
PROBLEMS
PV RT
V=
ZAID YAHYA
11-CH-74
¯ ¿∗N∗m 2 ∗1.01325 ¯ ¿m J ∗1003 cm3 101325 N mol∗K∗12 1m3 0.928∗8.314 J∗298.15 K V= ¿
ZRT P
3
V =1916.8
cm Answer mol
(d) From table 3.1
σ =1, Ω=0.08664, ε=0,ψ=0.42748,α ( T r )=α SRK ( T r ; ω )
[ {
(
α SRK ( T r ; ω )= 1+ ( 0.480+ 1.574 ω−0.176 ω2 ) 1−T r
[ {
(
2
α SRK ( T r ; ω )= 1+ ( 0.480+1.574∗0.087−0.176∗0.087 ) 1−1.056
1 2
1 2
2
)}]
2
) }]
2
α SRK ( T r ; ω )=[ 0.9828 ]
α SRK ( T r ; ω )=0.966 →(ii i ' ) Now
q=
ψα ( T r ) ΩT r
q=
0.42748∗0.966 0.08664∗1.056
'
q=4.515 →(ii i )
Put (i’) and (iii’) in (5)
Z =1+ 0.0195−4.515∗0.0195
Z−β ( Z + ϵ β )( Z +σβ )
Assume
Z =0.928
0.928=1.0195−0.08803
0.928−0.0195 0.9 ( 0.9+ 0.0195 )
0.928=1.0195−0.2383∗1.36
Since
L. H . S=R . H . S
72
0.928=0.928
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Therefore,
Z =0.928 Answer
We know that
Z=
PV RT
V=
¯ ¿∗N∗m ∗1.01325 ¯ ¿ m2 J ∗1003 cm3 101325 N mol∗K∗12 1m3 0.928∗8.314 J∗298.15 K V= ¿
ZRT P
cm3 V =1917 Answer mol
(e) From table 3.1
σ =1+ √2=2.41, Ω=0.07780, ε=1−√ 2=−0.414,ψ =0.45724, α ( T r )=α SRK ( T r ; ω ) Now
β=Ω
β=
0.07780∗0.238 1.056
Pr Tr
β=0.0175 →(iv ' )
[ {
(
α SRK ( T r ; ω )= 1+ ( 0.37464 +1.54226 ω−0.26992 ω2 ) 1−T r
[ {
2
(
1 2
2
)}]
α SRK ( T r ; ω )= 1+ ( 0.37464+ 1.54226∗0.087−0.26992∗0.087 ) 1−1.056
2
α SRK ( T r ; ω )=[ 0.986 ]
α SRK ( T r ; ω )=0.9722
Now
q=
73
ψα ( T r ) ΩT r
q=
0.42748∗0.9722 0.08664∗1.056
q=4.542 →(v ' )
1 2
2
) }]
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Put (iv’) and (v’) in (5)
Z =1+ 0.0175−4.542∗0.0175
Z−β ( Z + ϵ β )( Z+ σβ )
Assume
0.92=1.0175−0.07949
Z =0.92
0.92−0.0175 ( 0.92−0.414∗0.0175 ) ( 0.92+ 2.41∗0.0175 )
0.92=1.0175−0.07949∗1.027
0.92 ≈ 0.93 Since
L. H . S ≈ R . H . S Therefore,
Z =0.92 Answer
We know that
Z=
PV RT
V=
ZRT P
¯¿∗N∗m ∗1.01325 ¯¿ m2 J ∗1003 cm3 101325 N mol∗K∗12 1m3 0.92∗8.314 J∗298.15 K V= ¿
3
V =1900.4
cm Answer mol
Problem 3.33: Calculate Z and V for ethane at 50 oC and 15 bars by the following equations: a) The truncated virial equation [Eq. (3.40)] with the following experimental values of virial coefficients: 3 −1 6 −2 B=−156.7 cm mol C=9650 cm mol b) The truncated virial equation [Eq.(3.38)], with a value of B from the generalized Pitzer correlations [Eq. (3.63)] c) The Redlich/Kwong equation d) The Soave/Redlich/Kwong equation e) The Peng/Robinson equation. Given Data:
74
August 20, 2013
PROBLEMS
ZAID YAHYA
Temperature=T =50 ℃
11-CH-74
T =323.15 K
T =( 50+273.15 ) K
Pressure=P=15 ¯¿
Solution: (a) 3
B=−156.7 cm mol
6
−1
−2
C=9650 cm mol
Given equation is
Z =1+
B C + V V2 PV B C =1+ + 2 RT V V
V=
RT B C 1+ + 2 → ( 1 ) P V V
(
)
mol∗K∗15∗¯¿∗N∗m ∗1.01325 ¯¿ m2 J ∗1003∗cm 3 101325∗N 1 m3 RT 8.314∗J∗323.15 K = ¿ P
RT cm3 =2065.68 V mol
Put in (1)
V =1791
cm 3 B C 1+ + 2 mol V V
(
)
Assume
cm3 V =1625 mol Therefore
1625
75
cm3 cm3 156.7 9650 =1791 1− + mol mol 1625 16252
(
)
1625
cm3 cm3 ( =1791 0.9072 ) mol mol
1625
cm3 cm3 =1625 mol mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Since
L. H . S=R . H . S Therefore 3
V =1625
cm Answer mol
We know that
Z=
PV RT
15∗ ¯¿ 1625∗cm3∗mol∗K ∗J 8.314∗J∗323.15∗K∗mol ∗101325 N N∗m ∗1m3 2 1.01325 ¯¿ m Z= 1003 cm3
Z =0.907 Answer
(b)
Given equation 3.38 is
Z =1+
BP →( 2) RT
We know that
Reduced temperature=T r =
T Tc
T =T r T c → ( a )
Reduced Pressure=Pr =
Put (a) and (b) in (2)
Z =1+
B Pr Pc R T r Tc
Since
^ B Pc Reduced second virial coefficient =B= R Tc Therefore
76
P Pc
P=Pr Pc →(b)
August 20, 2013
PROBLEMS
ZAID YAHYA
Z =1+
11-CH-74
^B P r →(3) Tr
Also O ^ B=B +ω B1
Put in (3)
Z =1+ ( B O +ω B1 )
Pr →( 4) Tr
For ethylene (From Table B.1 Appendix B)
ω=0.1 →(i)
Critical temperature=T c =305.3 K
Critical pressure=Pc =48.72 ¯¿
Tr=
T 323.15 K = =1.058 →(ii) T c 305.3 K
48.72 ¯¿=0.308 →(iii ) ¯ 15 ¿¿ P Pr = =¿ Pc
Also we have o
B =0.083−
0.422 T r1.6
B o=0.083−
0.422 1.6 1.058
B o=−0.303 → ( iv )
B 1=0.139−
0.172 4.2 1.058
B 1=3.266∗10−3 →(v) Put (i), (ii), (iii), (iv) & (v) in (4)
Z =1+ (−0.303+ 0.1∗3.266∗10−3 )
0.308 1.058
Z =0.912 Answer
We know that
Z=
77
PV RT
V=
ZRT P
¯¿∗N∗m ∗1.01325 ¯¿ m2 J 3 3 ∗100 cm 101325 N mol∗K∗15 1 m3 0.912∗8.314 J∗323.15 K V= ¿
V =1633.36
cm3 Answer mol
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
(c)
The Redlich/Kwong equation is
Z =1+ β−qβ
Z−β → ( 5) ( Z + ϵ β ) ( Z +σβ )
Where
β=Ω
Pr Tr
From table 3.1
σ =1, Ω=0.08664, ε=0,ψ=0.42748,α ( T r )=T r
−1 2
Now
β=
0.08664∗0.308 1.058
'
β=0.0252 →(i )
Also
ψα ( T r ) q= ΩT r
q=
−1 2
0.42748∗1.058 0.08664∗1.058
q=4.533 →(ii ' )
Put (i’) and (ii’) in (5)
Z =1+ 0.0252−4.533∗0.0252
Z−β ( Z+ ϵ β )( Z+ σβ )
Assume
Z =0.906
0.906=1.0252−0.114
0.906−0.0252 0.906 ( 0.906+ 0.0252 )
0.906=1.0252−0.114∗1.044
Since
L. H . S=R . H . S Therefore, 78
0.906=0.906
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Z =0.906 Answer
We know that
Z=
PV RT
V=
¯¿∗N∗m 2 ∗1.01325 ¯¿ m J 3 3 ∗100 cm 101325 N mol∗K∗15 1 m3 0.906∗8.314 J∗323.15 K V= ¿
ZRT P
3
V =1622.7
cm Answer mol
(d) From table 3.1
σ =1, Ω=0.08664, ε=0,ψ=0.42748,α ( T r )=α SRK ( T r ; ω )
[ {
(
α SRK ( T r ; ω )= 1+ 0.480+1.574 ω−0.176 ω2 1−T r
[ {
2
(
α SRK ( T r ; ω )= 1+ 0.480+1.574∗0.1−0.176∗0.1 1−1.058
1 2
1 2
2
)}]
2
) }]
2
α SRK ( T r ; ω )=[ 1+0.6374 ]
α SRK ( T r ; ω )=2.681 →(ii i' ) Now
q=
ψα ( T r ) ΩT r
q=
0.42748∗2.681 0.08664∗1.058
'
q=12.50 →(iii )
Put (i’) and (iii’) in (5)
Z =1+ 0.0252−12.50∗0.0252
Z−β ( Z + ϵ β ) ( Z +σβ )
Assume
Z =0.907
79
0.907=1.0252−0.315
0.907−0.0252 0.907 ( 0.907+0.0252 )
0.907=1.0252−0.315∗1.0429
0.695=0.695
August 20, 2013
PROBLEMS
ZAID YAHYA
11-CH-74
Since
L. H . S=R . H . S Therefore,
Z =0.695 Answer
We know that
Z=
PV RT
V=
ZRT P
¯¿∗N∗m 2 ∗1.01325 ¯¿ m J ∗1003 cm3 101325 N mol∗K∗12 1m3 0.695∗8.314 J∗298.15 K V= ¿
3
V =1435.6
cm Answer mol
(e) From table 3.1
σ =1, Ω=0.07780, ε=0,ψ=0.45724,α ( T r )=α SRK ( T r ; ω ) Now
β=Ω
β=
0.07780∗0.238 1.056
Pr Tr
β=0.0175 →(iv ' )
[ {
(
α SRK ( T r ; ω )= 1+ 0.37464 +1.54226 ω−0.26992ω 2 1−T r
1 2
)}]
2
2 2 α SRK ( T r ; ω )=[ 1+ {0.37464+1.54226∗0.087−0.26992∗0.087 ( 1−1.056 ) } ]
2
α SRK ( T r ; ω )=[ 1+0.509 ] Now
80
α SRK ( T r ; ω )=2.277
2
August 20, 2013
PROBLEMS
ZAID YAHYA
q=
ψα ( T r ) ΩT r
q=
0.42748∗2.277 0.08664∗1.056
11-CH-74
q=10.64 →( v ' )
Put (iv’) and (v’) in (5)
Z =1+ 0.0175−10.64∗0.0175
Z−β ( Z + ϵ β )( Z+ σβ )
Assume
Z =0.793
0.793=1.0175−0.1862
0.793−0.0175 0.793 ( 0.793+0.0175 )
0.793=1.0175−0.1862∗1.2066
0.793=0.793
Since
L. H . S=R . H . S Therefore,
Z =0.793 Answer
We know that
Z=
81
PV RT
V=
ZRT P
¯ ¿∗N∗m ∗1.01325 ¯ ¿ m2 J ∗1003 cm3 101325 N mol∗K∗12 1m3 0.793∗8.314 J∗298.15 K V= ¿
V =1638.1
cm 3 Answer mol
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