This document discusses thermodynamic properties of fluids, including:
1) Derivations of equations relating the primary thermodynamic properties of pressure, volume, temperature, internal energy, and entropy for homogeneous phases and fluids.
2) Calculations of changes in enthalpy, entropy, and internal energy based on changes in pressure and temperature.
3) The thermodynamic properties of Gibbs energy and residual properties.
4) An example problem calculating the enthalpy and entropy of saturated isobutane vapor at a specified temperature and pressure using compressibility factor and ideal gas heat capacity data.
Excess property introduction
▪ Excess volume
▪ Excess gibbs free energy
▪ Entropy of mixing
▪ what is use of Residual property and Excess property
in thermodynamics
▪ Case study
▪ Thermo-calc demo
▪ conclusion
Excess property introduction
▪ Excess volume
▪ Excess gibbs free energy
▪ Entropy of mixing
▪ what is use of Residual property and Excess property
in thermodynamics
▪ Case study
▪ Thermo-calc demo
▪ conclusion
This presentation gives you information om Clausius Statement, its proof, Entropy change for Open System and reversible and irreversible processes with simple explanation and day to day examples.
Thermodynamics II course taught at air university Islamabad by Sijal Ahmed. In this lecture we have discussed about the gas-gas mixtures in very much details including how to find out the different thermodynamics properties for mixtures.
Excess gibbs free energy models,MARGULES EQUATION
,REDLICH-KISTER EQUATION,VAN LAAR EQUATION
,WILSON AND “NRTL” EQUATION
,UNIversal QUAsi Chemical equation
Slides for the eLearning course Separation and purification processes in biorefineries (https://open-learn.xamk.fi) in IMPRESS project.
Section: Distillation
Subject: 1.1 Vapor Liquid Equilibrium
This presentation is made to provide the overall conceptual knowledge on Chilton Colburn Analogy. It includes basis, importance, assumption, advantages, limitations and applications in addition to the derivation. Make It Useful!
This presentation gives you information om Clausius Statement, its proof, Entropy change for Open System and reversible and irreversible processes with simple explanation and day to day examples.
Thermodynamics II course taught at air university Islamabad by Sijal Ahmed. In this lecture we have discussed about the gas-gas mixtures in very much details including how to find out the different thermodynamics properties for mixtures.
Excess gibbs free energy models,MARGULES EQUATION
,REDLICH-KISTER EQUATION,VAN LAAR EQUATION
,WILSON AND “NRTL” EQUATION
,UNIversal QUAsi Chemical equation
Slides for the eLearning course Separation and purification processes in biorefineries (https://open-learn.xamk.fi) in IMPRESS project.
Section: Distillation
Subject: 1.1 Vapor Liquid Equilibrium
This presentation is made to provide the overall conceptual knowledge on Chilton Colburn Analogy. It includes basis, importance, assumption, advantages, limitations and applications in addition to the derivation. Make It Useful!
Drilling Hydraulic of Compressible and In-compressible Drilling FluidAmir Rafati
Incompressible Fluids
1. static Well Conditions
• Hydrostatic Pressure in Liquid Columns
• Hydrostatic Pressure in Mixed Columns
• Kick Identification
• Buoyancy and Effect of Buoyancy on Buckling
2. Non-static Well Conditions
• Flow Through Jet Bits
• Shear Stress V.S. Shear Rate (Laminar)
3. Rheological Models
• Newtonian
• Non-Newtonian
• Rotational Viscometer
• Initial Circulating of Well
4. Laminar Flow In Pipes & annulus
• Newtonian Flow In Pipes & annulus
• Newtonian Flow In Pipes & annulus (As a Slot)
5. Turbulent Flow In Pipes & annulus
• Moody Diagram
• Critical Velocity
• Hanks Turbulence Criterion
6. Extension Equations For Flow
• Hydraulic Radius
• Apparent Viscosity
7. Jet Nozzle Size Selection
• Pressure loss Simplification
• Maximum Nozzle Velocity
• Maximum Bit Hydraulic Horsepower
• Maximum Jet Impact Force
• Minimum needed annular Velocity
8. Surge and swab pressure of Vertical Pipe Move
9. Particle Slip Velocity
10. Known Cleaning Needs
Compressible Fluids
11. Basic Technology
• Introduction
• Surface Equipment
• Down hole Equipment
• Compressors
• Shallow Well Drilling Applications
12. Circulation Systems
• Reverse Circulation
• Direct Circulation
13. Comparison of Mud and Air Drilling
• Pressure profile
• Heat capacity
• Density profile
• Kinetic energy profile
14. Surface Equipment Summery
• Drilling Location
• Flow Line to the Rig
• Wellhead Equipment
• Flow Line from Rig
15. Downhole Equipment Summery
• Rotary Drill String
• Drill Bits
• Bottom hole Assembly
• Drill Pipe
• Safety Equipment
• Drill String Design
16. Compressors type Nominations
• Continuous Flow
• Intermittent Flow
17. Power Requirements
• Single Stage Shaft
• Multistage Shaft
• Prime Mover Input
18. Reciprocating Compressor Unit
19. Shallow Well Drilling Applications
• Shallow Well Drilling Planning
• Direct Circulation
• Reverse Circulation
• Direct Circulation Based on Weight Rate of Flow
• General Derivation
• Wet and Dry Air and Gas Drilling Model
• Unstable and Stable Foam Drilling
• Aerated Fluid Drilling Model
20. Direct Circulation Hydraulic Sections
• the injection pressure into the top of the drill string
• pressure at bottom of drill pipe inside the drill string
• pressure at bottom of drill collars inside the drill string
• pressure above drill bit inside the drill string
• pressure at bottom of drill collars in the annulus
• pressure at bottom of drill pipe in the annulus
• pressure at the bottom of casing in the annulus
• pressure at the top of the annulus
21. Air and Gas Drilling Models
• Deep Well Drilling Planning
• Minimum Volumetric Flow Rate
• Terminal Velocities
• Injection Pressure and Selection of Compressor Equipment
• Prime Mover Fuel Consumption
• Water Injection
• Drilling and Completion Problems
22. Major & Minor Loss & Injection Pressure
• Non-Frictional Approximation
• Frictional Approximation
Overview of the fundamental roles in Hydropower generation and the components involved in wider Electrical Engineering.
This paper presents the design and construction of hydroelectric dams from the hydrologist’s survey of the valley before construction, all aspects and involved disciplines, fluid dynamics, structural engineering, generation and mains frequency regulation to the very transmission of power through the network in the United Kingdom.
Author: Robbie Edward Sayers
Collaborators and co editors: Charlie Sims and Connor Healey.
(C) 2024 Robbie E. Sayers
Saudi Arabia stands as a titan in the global energy landscape, renowned for its abundant oil and gas resources. It's the largest exporter of petroleum and holds some of the world's most significant reserves. Let's delve into the top 10 oil and gas projects shaping Saudi Arabia's energy future in 2024.
Hierarchical Digital Twin of a Naval Power SystemKerry Sado
A hierarchical digital twin of a Naval DC power system has been developed and experimentally verified. Similar to other state-of-the-art digital twins, this technology creates a digital replica of the physical system executed in real-time or faster, which can modify hardware controls. However, its advantage stems from distributing computational efforts by utilizing a hierarchical structure composed of lower-level digital twin blocks and a higher-level system digital twin. Each digital twin block is associated with a physical subsystem of the hardware and communicates with a singular system digital twin, which creates a system-level response. By extracting information from each level of the hierarchy, power system controls of the hardware were reconfigured autonomously. This hierarchical digital twin development offers several advantages over other digital twins, particularly in the field of naval power systems. The hierarchical structure allows for greater computational efficiency and scalability while the ability to autonomously reconfigure hardware controls offers increased flexibility and responsiveness. The hierarchical decomposition and models utilized were well aligned with the physical twin, as indicated by the maximum deviations between the developed digital twin hierarchy and the hardware.
NO1 Uk best vashikaran specialist in delhi vashikaran baba near me online vas...Amil Baba Dawood bangali
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Student information management system project report ii.pdfKamal Acharya
Our project explains about the student management. This project mainly explains the various actions related to student details. This project shows some ease in adding, editing and deleting the student details. It also provides a less time consuming process for viewing, adding, editing and deleting the marks of the students.
Industrial Training at Shahjalal Fertilizer Company Limited (SFCL)MdTanvirMahtab2
This presentation is about the working procedure of Shahjalal Fertilizer Company Limited (SFCL). A Govt. owned Company of Bangladesh Chemical Industries Corporation under Ministry of Industries.
2. Property relations for homogeneous phases
First law for a closed system d(nU) = dQ + dW
a special reversible process
rev rev d(nU) = dQ + dW
dW Pd(nV) rev = - dQ Td(nS) rev =
d(nU) = Td(nS) - Pd(nV )
Only properties of system are involved:
It can be applied to any process in a closed system (not necessarily
reversible processes).
The change occurs between equilibrium states.
3. The primary thermodynamic properties: P,V, T,U, and S
The enthalpy: H ºU + PV
The Helmholtz energy: A ºU -TS
The Gibbs energy: G º H -TS
For one mol of homogeneous fluid of constant composition:
dU = TdS - PdV
d(nU) = Td(nS) - Pd(nV )
dH = TdS +VdP
dA = -PdV - SdT
P
= - ¶ ÷ø
ö çè
÷ø
æ
¶
S V S
T
¶
æ
ö ¶
V
çèV
= ¶ ÷ø
ö çè
÷ø
æ
¶
S P S
T
¶
æ
ö ¶
P
çè
S
= ¶ ÷ø
ö çè
÷ø
æ
¶
¶
ö çè
V T V
P
æ
¶
T
S
V
= - ¶ ÷ø
ö çè
¶
dG =VdP - SdT Maxwell’s equations
P T P
T
÷ø
æ
¶
æ
ö ¶
çè
4. Enthalpy, entropy and internal energy change calculations f (P,T)
= ¶ dP
dP
dT H
+ ¶ ÷ø
æ
ö ¶
P
çè
dH H
T
÷ø
P T
æ
ö ¶
çè
dT S
+ ¶ ÷ø
æ
ö ¶
P
çè
dS = ¶
S
T
÷ø
P T
æ
ö ¶
çè
dH = TdS +VdP
P
H = ÷ø
P
C
æ
ö ¶
T
çè
¶
V
T S
= ¶ ÷ø
æ
ö ¶
P
çè
H
P
+ ÷ø
T T
¶
æ
ö ¶
çè
¶
æ
H
= ¶ ÷ø
= + ¶
T S
ö çè
P ÷ ÷ø
V dP
dH C dT T S
P
T
ö
ç çè
+ ÷ø
æ
¶
S
= - ¶ ÷ø
ö çè
P T P
V
T
÷ø
æ
¶
¶
æ
ö ¶
çè
dP
æ
dH = C dT + V - T ¶
V
ö çè
P ÷ ÷ø
T
P
ö
ç çè
÷ø
æ
¶
S C
P
T
¶
T
= ÷ø
P
æ
ö ¶
çè
= - ¶ ÷ø
ö çè
dP
V
V
¶
= - ¶
æ
ö ¶
T
çè
dS C dT
T
P
P ÷ø
P P T
T
÷øö çè
æ
¶
æ
ö ¶
çè
S
P T P
T
÷ø
æ
¶
æ
ö ¶
çè
H ºU + PV
V
P V
+ ¶ ÷ø
æ
ö ¶
P
çè
U
= ¶ ÷ø
æ
ö ¶
P
çè
H
P
+ ÷ø
T T T
¶
æ
ö ¶
çè
P V
T V
- ¶ ÷ø
ö çè
= - ¶ ÷ø
P
P
T T T U
P
÷ø
æ
¶
æ
ö ¶
çè
¶
æ
ö ¶
çè
5. Determine the enthalpy and entropy changes of liquid water for a
change of state from 1 bar and 25°C to 1000 bar and 50°C. The data
for water are given.
H1 and S1 at 1 bar, 25°C
H2 and S2 at 1 bar, 50°C H3 and S3 at 1000 bar, 50°C
dP
æ
dH = C dT + V - T ¶
V
ö çè
P ÷ ÷ø
T
P
ö
ç çè
÷ø
æ
¶
( H 75.310(323.15 298.15) 1 (513 10 -
)(323.15) ) (18.204)(1000 1)
3400J /mol
dP
V
= - ¶
æ
ö ¶
T
çè
dS C dT
T
P
P ÷ø
dH C dT ( T )VdP P = + 1-b
( ) (1 ) ( ) 2 1 2 2 1 H C T T T V P P P D = - + - b -
V
V
T
b = ÷ø
P
¶
æ
ö ¶
çè
volume expansivity
S C T P D = - b -
2 V P P
T
ln ( ) 2 1
1
10
6
D = - + - ´ - =
( 513 10 -
) S (18.204)(1000 1)
5.13J /mol
10
75.310ln 323.15
298.15
6
D = - ´ - =
6. Internal energy and entropy change calculations f (V,T)
= ¶ dV
dV
dT U
+ ¶ ÷ø
æ
ö ¶
V
çè
dU U
ö T
çè
÷ø
V T
æ
¶
dT S
+ ¶ ÷ø
æ
ö ¶
V
çè
dS = ¶
S
ö T
çè
÷ø
V T
æ
¶
V
U = ÷ø
ö çè
V
C
æ
¶
T
¶
T S
U
= ¶ ÷ø
æ
ö ¶
çè
¶
V ÷ ÷ø ö
- ÷ø
P dV
æ
dU = C dT + T ¶
S
ö V
çè
T
ç çè
- ÷ø
æ
¶
P
= - ¶ ÷ø
ö çè
T V T
S
¶
V
÷ø
æ
¶
æ
ö ¶
çè
æ
= + ¶
ö çè
V ÷ ÷ø
P dV
dU C dT T P
T
V
ö
ç çè
- ÷ø
æ
¶
T S
= ¶ ÷ø
ö çè
S C
V
T
¶
ö T
çè
= ÷ø
V
æ
¶
= - ¶ ÷ø
ö çè
dV
S
P
¶
= + ¶
ö çè
V ÷ø
T
dS C dT
T
V
æ
¶
P
V
V
T T
æ
ö ¶
çè
V V T
U
T
÷ø
æ
¶
¶
æ
ö ¶
çè
P
T V T
V
÷ø
æ
¶
æ
ö ¶
çè
7. Gibbs energy G = G (P,T)
dG =VdP - SdT
dT
d G dG G
2
RT
º 1 - ÷ø
ö çè
RT RT
æ
Thermodynamic property of great potential utility
dG =VdP - SdT
dT
÷ø
çè
d æ
G ö º V
dP - H
RT
RT
RT
2 G º H -TS
dT
dP G RT
+ ¶ ÷ø
æ ( / ) ( / )
ö T
çè
G RT
P
d G
RT
÷ø
æ
¶
T P
æ
ö ¶
çè
= ¶ ÷ø
ö çè
G RT
= ¶( / )
ö çè
T P
V
RT
÷ø
æ
¶
T G RT
= - ¶( / )
ö çè
P T
H
RT
÷ø
æ
¶
G/RT = g (P,T)
The Gibbs energy serves as a generating function
for the other thermodynamic properties.
8. Residual properties
• The definition for the generic residual property:
M R º M -Mig
– M and Mig are the actual and ideal-gas properties,
respectively.
– M is the molar value of any extensive thermodynamic
properties, e.g., V, U, H, S, or G.
• The residual Gibbs energy serves as a generating
function for the other residual properties:
dT
ö
R R R
dP H
RT
V
RT
æ
d G
RT
2 - = ÷ ÷ø
ç çè
9. R R
= ÷ ÷ø
æ
æ const T dP
dT
ö
R R R
dP H
RT
V
RT
d G
RT
2 - = ÷ ÷ø
ç çè
V
RT
d G
RT
ö
ç çè
= òR P R
dP
V
RT
G
RT
0
RT
P
V R =V -V ig = ZRT -
P
= - ¶( / )
ö çè
( 1) P T
= ò - R P
Z dP
P
G
RT
0
T G RT
H
RT
÷ø
æ
¶
T Z
= - ¶ P
æ
ö ¶
çè
ò ÷ø
P
R
dP
P
T
H
RT
0
dP
T Z
= - ¶ P P
æ
ö ¶
çè
Z dP
ò ò - - ÷ø
P
R
P
P
T
S
R
0 0
( 1)
S R R G
R
RT
H
RT
R
= -
const T
const T
Z = PV/RT: experimental measurement .Given PVT data or an appropriate equation
of state, we can evaluate HR and SR and hence all other residual properties.
10. { }
þ ý ü î í ì
H = H + H = H + C dT + - RT ¶
Z
ö çè
÷ø
dP
0
H R ICPH T T A B C D RT Z
= + ´ + - ¶
{ }
{ ( )}
{ ( )}
þ ý ü
î í ì
( , ; , , , )
H C T T RT Z
= + - + - ¶
ö çè
dP
dP
0
2
0 0
H R MCPH T T A B C D T T RT Z
= + ´ - + - ¶
ö çè
÷ø
æ
¶
þ ý ü
î í ì
÷ø
æ
¶
þ ý ü
î í ì
÷øö çè
æ
¶
æ
¶
ò
ò
ò
ò ò
P
P
ig
P
P
H
ig
P
ig
P
P
ig
P
P
T
T
ig
P
ig R ig
dP
P
T
P
T
P
T
P
T
0
2
0 0 0
0
2
0 0
0
2
0
( , ; , , , )
þ ý ü
R T Z
+ - ¶
ö çè
dP
R P
S S S S C dT
ò ò ò
ln ( 1)
R T Z
+ - ¶
ö çè
dP
Z dP
ò ò
0
( , ; , , , ) ln ( 1)
ln ln ( 1)
î í ì
Z dP
R T Z
dP
+ - ¶
ö çè
Z dP
Z dP
dP
- - ÷ø
æ
¶
þ ý ü
S R ICPS T T A B C D R P
R T Z
+ - ¶
ö çè
R P
S C T
î í ì
î í ì = + ´ -
þ ý ü
- - ÷ø
æ
¶
þ ý ü
î í ì
= + -
þ ý ü
î í ì
- - ÷ø
æ
¶
þ ý ü
î í ì
= + ´ -
þ ý ü
î í ì
- - ÷ø
æ
¶
þ ý ü
î í ì
= + = + -
ò ò
ò ò
P P
P
S ig
R MCPS T T A B C D T
P P
P
S
ig
P
ig
P P
P
ig
P P
P
T
T
ig
P
ig R ig
P
P
T
R P
P
T
P
P
T
P
T
P
P
T
P
P
P
T
P
T
0 0
0 0
0 0
0 0
0 0
0
0 0
0
0 0
0 0
0
0
( , ; , , , ) ln ln ( 1)
11. Calculate the enthalpy and entropy of saturated isobutane vapor at 360
K from the following information: (1) compressibility-factor for
isobutane vapor; (2) the vapor pressure of isobutane at 360 K is 15.41
bar; (3) at 300K and 1 bar, Hig = 18115 J /mol Sig = 295.976 J /mol ×K 0 0
(4) the
ideal-gas heat capacity of isobutane vapor:
Cig / R =1.7765 + 33.037´10-3
T
P
T Z
= - ¶ P
æ
ö ¶
çè
ò ÷ø
P
R
dP
P
T
H
RT
dP
T Z
= - ¶ P P
æ
ö ¶
çè
Z dP
S
0 ò ò - - ÷ø
P
R
P
P
T
R
0 0
( 1)
Z
¶
Graphical integration requires plots of P and (Z-1)/P vs. P.
T
/ ÷ø
P
æ
ö ¶
çè
dP
T Z
= - ¶ - òP
(360)(26.37 10 4 ) 0.9493
0
ö çè
- = ´ - = ÷ø
æ
¶
P
R
P
T
H
RT
dP
T Z
= - ò ¶ òP P
ö çè
Z dP
- = - - - = - - ÷ø
( 1) 0.9493 ( 0.02596) 0.6897
æ
¶
0 0
P
R
P
P
T
S
R
H R = -2841.3J /mol
S R = -5.734J /mol ×K
H = { Hig + R ´ ICPH(300,360;1.7765,33.037E - 3,0.0,0.0) } + H R =
21598.5 J 0 mol
{ } mol K
S Sig R ICPS E R S R J
×
(300,360;1.7765,33.037 3,0.0,0.0) ln 15.41 0
= + ´ - - + = 286.676
1
12. Residual properties by equation
of state
• If Z = f (P,T):
T Z
= - ¶ P
æ
ö ¶
çè
ò ÷ø
dP
T Z
= - ¶ P P
æ
ö ¶
çè
R
Z dP
S
÷ø
ò - ò - 0 P
R
dP
P
T
H
RT
0 0
P
P
P
T
R
( 1)
• The calculation of residual properties for gases
and vapors through use of the virial equations and
cubic equation of state.
13. Use of the virial equation of state
Z -1 = BP
RT
= ò - R P
Z dP
P
G
RT
0
( 1)
two-term virial equation
BP
RT
GR
RT
=
T Z
= - ¶ P
æ
ö ¶
çè
ò ÷ø
P
R
dP
P
T
H
RT
= - ¶ P
BP
æ +
ö ¶
çè
H
Z -1 = BP
0 ò ÷ø
P
R
dP
P
RT
T
T
RT
0
(1 )
ö
T æ
P
ö çè
B
dB
1
ö çè
ò ÷ ÷ø
ç çè
÷ø
æ - ÷ø
= - æ P
P
R
dP
P
T
dT
R T
H
RT
0 2
RT
dB
B
ö çè
÷ø
P
= æ -
dT
T
R
H R
RT
S R R G
R
RT
H
RT
R
= -
P
dB
R
dT
S R
RT
= -
14. Z -1 = Br +Cr 2
Three-term virial equation
= ò - R P
Z dP
P
G
RT
0
( 1)
= 2 r + 3 r 2 -
B C Z
GR
RT
ln
2
T Z
= - ¶ P
æ
ö ¶
çè
ò ÷ø
P
R
dP
P
T
H
RT
ù
T é
B
dC
C
r 1 r
dB
= æ - 2
ö çè
ö çè
H R
0 úû
êë
÷ø
æ - + ÷ø
2
dT
T
dT
T
RT
S R R G
R
RT
H
RT
R
= -
P = ZrRT
Application up to moderate pressure
15. Use of the cubic equation of state
• The generic cubic equation of state:
a T
( )
V b V b
( )( )
P RT
V b
+e +s
-
-
=
1
q r
b
b b
b
r + +
1 (1 )(1 )
Z
er sr
-
-
=
q º a(T)
bRT
ò r (Z -1) d r
= -ln(1- r
b) - qI
0
r
I
Z = - ÷ø
d dq
dT
¶ òr
æ
ö ¶
T
çè
r
r r
0
const T
I ò d ( r
b)
+ +
b b
º r
er sr
0 (1 )(1 )
qI
é
Z d T
1 lna ( )
= - + -1
d T
H
RT
r
r
R
ù
úû
êë
ln
é
Z d T
ù
ln b lna ( )
( ) qI
= - + -1
d T
S
R
r
r
R
úû
êë
ln
b º bP
RT
16. Find values for the residual enthalpy HR and the residual entropy SR
for n-butane gas at 500 K and 50 bar as given by Redlich/Kwong
equation.
T = 500 = 1.317
r 1.176
425.1
= 50 = r P = W = 0.09703
37.96
b P ( ) = 3.8689
r
T
r
q = Y
a T
r
T
W
r
Z q Z
= + - -
b b b
Z Z
+ +
( )( )
1
eb sb
e = 0
s =1 Z = 0.685
qI
I ò d ( r
b)
+ +
é
Z d T
1 lna ( )
= - + -1
d T
H
RT
r
r
R
ù
úû
êë
ln
é
Z d T
ù
ln b lna ( )
( ) qI
= - + -1
d T
S
R
r
r
R
úû
êë
ln
const T
b b
º r
er sr
0 (1 )(1 )
ö
æ
+
sb
I Z
13247 . 0 ln 1 = ÷ ÷ø
ç çè
+
-
=
eb
s e Z
H R = -4505 J
mol
S R J
mol ×
K
= -6.546
17. Two-phase systems
• Whenever a phase transition at constant
temperature and pressure occurs,
– The molar or specific volume, internal energy,
enthalpy, and entropy changes abruptly. The exception
is the molar or specific Gibbs energy, which for a pure
species does not change during a phase transition.
– For two phases α and β of a pure species coexisting at
equilibrium:
Ga = Gb
where Gα and Gβ are the molar or specific Gibbs energies of the individual phases
18. Ga = Gb dGa = dGb
dG =VdP - SdT
ab
a b
S
S S
dPsat
= D
= -
Va dPsat - Sa dT =V b dPsat - Sb dT a b
ab
V
V V
dT
D
-
dH = TdS +VdP DHab = TDSab
The latent heat of phase transition
ab
ab
H
= D
T V
dPsat
dT
D
The Clapeyron equation
DVab =V = RT
sat
v
P
Ideal gas, and Vl << Vg
H R d P
sat
ln
d T
(1/ )
D lv = -
The Clausius/Clapeyron equation
19. ab
ab
H
= D
T V
dPsat
dT
D
The Clapeyron equation: a vital connection between the properties of different phases.
P = f (T)
ln Psat = A- B For the entire temperature range from the triple point
T
to the critical point
Psat A B
ln = - The Antoine equation, for a specific temperature range
T +
C
= + + +
t t t t
-
t
1
ln
A B 1.5 C 3 D 6 Psat
r
The Wagner equation, over a wide
temperature range.
r t =1-T
20. Two-phase liquid/vapor systems
• When a system consists of saturated-liquid and
saturated-vapor phases coexisting in equilibrium,
the total value of any extensive property of the
two-phase system is the sum of the total properties
of the phases:
M = (1- xv )Ml + xvMv
– M represents V, U, H, S, etc.
– e.g., V = (1- xv )V v + xvV v
21. Thermodynamic diagrams and tables
• A thermodynamic diagram represents the temperature,
pressure, volume, enthalpy, and entropy of a substance on
a single plot. Common diagrams are:
– TS diagram
– PH diagram (ln P vs. H)
– HS diagram (Mollier diagram)
• In many instances, thermodynamic properties are reported
in tables. The steam tables are the most thorough
compilation of properties for a single material.
25. Superheated steam originally at P1 and T1 expands through a nozzle to an
exhaust pressure P2. Assuming the process is reversible and adiabatic, determine
the downstream state of the steam and ΔH for the following conditions:
(a) P1 = 1000 kPa, T1 = 250°C, and P2 = 200 kPa.
(b) P1 = 150 psia, T1 = 500°F, and P2 = 50 psia.
Since the process is both reversible and adiabatic, the entropy change
of the steam is zero.
(a) From the steam stable and the use of interpolation,
At P1 = 1000 kPa, T1 = 250°C:
H1 = 2942.9 kJ/kg, S1 = 6.9252 kJ/kg.K
At P2 = 200 kPa,
S2 = S1= 6.9252 kJ/kg.K < Ssaturated vapor,
the final state is in the two-phase liquid-vapor region:
S xv Sl xvSv 2 2 2 2 2 = (1- ) + xv xv2 2 6.9252 =1.5301(1- ) + 7.1268
0.9640 2 xv =
H H H 315.9 kJ 2 1 D = - = -
(1 0.964)(504.7) (0.964)(2706.3) 2627.0 2 kg H = - + =
26. (a) From the steam stable and the use of interpolation,
At P1 = 150 psia, T1 = 500°F:
H1 = 1274.3 Btu/lbm, S1 = 1.6602 Btu/lbm.R
At P2 = 50 psia,
S2 = S1= 1.6602 Btu/lbm.K > Ssaturated vapor,
the final state is in the superheat region:
T 283.28 F 2 =
H H H 99.0 Btu 2 1 D = - = -
lbm
H 1175.3 Btu / lbm 2 =
27. A 1.5 m3 tank contains 500 kg of liquid water in equilibrium with pure water
vapor, which fills the remainder of the tank. The temperature and pressure are
100°C, and 101.33 kPa. From a water line at a constant temperature of 70°C and
a constant pressure somewhat above 101.33 kPa, 750 kg of liquid is bled into
the tank. If the temperature and pressure in the tank are not to change as a result
of the process, how much energy as heat must be transferred to the tank?
d mU Energy balance: ( )cv = + ¢ ¢
Q H m
dt
d mU ( )cv = + ¢ cv
Q H dm
dt
dt
cv cv Q = D(mU) - H¢Dm
H =U + PV
cv cv cv Q = D(mH) - D(PmV ) - H¢Dm
cv cv cv Q = (m H ) - (m H ) - H¢Dm 2 2 1 1
At the end of the process, the tank still contains saturated liquid and
saturated vapor in equilibrium at 100°C and 101.33 kPa.
28. Q = (m H ) - m H - H¢Dm 2 2 cv () 1 1 cv cv H¢ = 293.0 kJ saturated liquid @70
C
kg
saturated liquid C
kJ Hlcv
= 419.1 @100
kg
saturated vapor C
Hv kJ
kg
cv
= 2676.0 @100
From the steam table, the specific volumes of saturated liquid and saturated
vapor at 100°C are 0.001044 and 1.673 m3/kg , respectively.
( ) 500(419.1) 1.5 (500)(0.001044) 1 1 1 1 1 1 = + = + - =
m H mlHl mvHv kJ
cv (2676.0) 211616
1.673
= 500 + 1.5 - (500)(0.001044) + = + mv ml2 2 1.5 =1.673 + 0.001044
m ml mv2 2 2 750
1.673
m H mlHl mvHv kJ
( )cv 524458 2 2 2 2 2 2 = + =
Q m H m H H m kJ ( )cv ( )cv cv 524458 211616 (750)(293.0) 93092 2 2 1 1 = - - ¢D = - - =
29. c r P = P P c r T = T T
T Z
= - ¶ P
æ
ö ¶
çè
ò ÷ø
P
R
dP
P
T
H
RT
0
dP
T Z
= - ¶ P P
æ
ö ¶
çè
Z dP
ò ò - - ÷ø
P
R
P
P
T
S
R
0 0
( 1)
ö
æ
¶
T Z
= - ¶ r
ò ÷ ÷ø
ç çè
r
P
dP
r
r
r P
r
R
c
P
T
H
RT
0
2
ö
æ
¶
dP
T Z
= - ¶ r r
Z dP
P r
ò ò - - ÷ ÷ø
ç çè
r
P
r
r
r
r P
r
R
P
P
T
S
R
0 0
( 1)
Z = Z 0 +wZ1
ù
ú ú
û
é
T Z
dP
T Z
= - ò ¶ ò r
- - ¶
ê ê
ë
ö
÷ ÷ø
æ
¶
ç çè
ù
ú ú û
é
ê ê
ë
ö
÷ ÷ø
æ
¶
ç çè
r
r
r
P
dP
r
r
r P
r
P
r
r
r P
r
R
c
P
T
P
T
H
RT
0
1
2
0
0
2 w
ù
ú ú
û
é
dP
T Z
Z dP
dP
T Z
= - ò ¶ ò - - ò r ¶
ò r
ê ê
ë
ö
Z dP
P r
- - ÷ ÷ø
æ
¶
ç çè
ù
ú ú
û
é
ê ê
ë
ö
P r
- - ÷ ÷ø
æ
¶
ç çè
r
r r
r
P
r
r
r
r P
r
P
r
r
r
r P
r
R
P
P
T
P
P
T
S
R
0
1
0
1
0
0
0
0
( 1) w ( 1)
( ) ( ) ( , , )
é
H
0 H
R
1
= +w
HRB TR PR OMEGA
RT
RT
( ) ( ) ( , , )
H
R
RT
c
c
R
c
=
ù
ú úû
ê êë
é
0 1
= +w SRB TR PR OMEGA
Table E5 ~ E12
S R R S
R
R
S
R
R
=
ù
ú úû
ê êë
30. T R
T
0 = + ò +
H Hig 2
C ig
dT H2 0 P
2
T R
T
0 = + ò +
H Hig 1
C ig
dT H1 0 P
1
T R R
T
D = ò + -
H 2
C ig
dT H HP 2 1
1
S S C dT R P
2
T R
T
= + ò - ln +
ig S
ig
P
2
P
T
0
2 0
2
0
S S C dT R P
1
T R
T
= + ò - ln +
ig S
ig
P
1
P
T
0
1 0
1
0
ig
P H C T T H H2 1 2 1 D = ( - ) + -
R R
S C dT R P
2 1
T R R
T
D = ò - ln + -
ig
P S S
2 2
1
P
T
1
H
S C ig
P S S
P 2 1
R R
D = ln 2 + -
S
P
1
31. Estimate V, U, H, and S for 1-butene vapor at 200°C and 70 bar if H and S are
set equal to zero for saturated liquid at 0°C. Assume that only data available are:
T K c = 420 P bar c = 40.43 w = 0.191 T 266.9K (nomal boiling pt.) n =
Cig / R 1.967 31.630 10 3T 9.837 10 6T 2
P
= + ´ - - ´ -
=1.127 r T =1.731 r P
0 1
Z = Z +wZ
= +
0.485 (0.191)(0.142)
0.512
=
cm
mol
V ZRT
P
3
= = 287.8
Assuming four steps:
(a) Vaporization at T1 and P1 = Psat
(b) Transition to the ideal-gas state at (T1, P1)
(c) Change to (T2, P2) in the ideal-gas state
(d) Transition to the actual final state at (T2, P2)
Fig 6.7
33. Step (a)
ln Psat = A- B
T
ln1.0133 = A- B
266.9
ln 40.43 = A- B
420
For = 273.15K,
Psat = 1.2771 bar
9.979
lv
n
H
D = -
1.092(ln 1.013) =
0.930
-
rn
c
n
T
P
RT
The latent heat at normal boiling point:
The latent heat at 273.15 K:
0.38
æ
-
= 1
-
1
ö
÷ ÷
ø
ç ç
è
H
D
D
T
r
rn
lv
lv
n
T
H
DHlv = 21810 J
mol
DHab = TDSab
Slv J
mol ×
K
D = 79.84
Step (b) = 0.650 r T = 0.0316 r P
( ) ( ) ( , , ) 0.0985
é
0 1
= + HRB TR PR OMEGA
= = -
ù
ú úû
ê êë
H
R
RT
H
RT
H
R
RT
c
c
R
c
w
( ) ( ) ( , , ) 0.1063
é
0 1
= + SRB TR PR OMEGA
= = -
ù
ú úû
S R R R
ê êë
S
R
S
R
R
w
H R 344 J 1 - =
mol
S R J
mol ×
K
- = 0.88 1
34. Step (c)
DHig = 8.314´ ICPH(273.15,473.15;1.967,31.630E -3,-9.837E - 6,0.0) = 20564 J
mol
8.314 (273.15,473.15;1.967,31.630 3, 9.837 6,0.0) 8.314ln 70
Sig ICPS E E
D = ´ - - - -
J
mol ×
K
=
22.18
1.2771
Step (d) =1.127 r T =1.731 r P
( ) ( ) 2.430
é
= +
0 1
= -
ù
ú úû
H w
ê êë
R
c
c
R
R
c
H
RT
H
RT
RT
( ) ( ) 1.705
é
= +
0 1
= -
ù
ú úû
S R R R
ê êë
S
R
S
R
R
w
H R 8485 J 2 = -
mol
S R J
mol ×
K
= -14.18 2
H = DH = 21810 - (-344) + 20564 -8485 = 34233 J
mol
S S J
mol ×
K
= D = 79.84 - (-0.88) + 22.18 -14.18 = 88.72
Total
U = H - PV= 34233- (70)(287.8) /10 = 32218 J
mol
35. Gas mixtures
• Simple linear mixing rules
w ºå
yw i i ºå
i
Pc i ci T y T ºå
i
Pc i ci P y P
i
Estimate V, HR, and SR for an equimolar mixture of carbon dioxide and propane
at 450K and 140 bar
T y T K
= (0.5)(304.2) + (0.5)(369.8) = 337
Pc ºå i ci i
P y P bar
Pc i ci ºå = (0.5)(73.83) + (0.5)(42.48) = 58.15 = 2.41 pr P
i
=1.335 pr T Z 0 = 0.697
Z1 = 0.205
188 . 0 ) 152 . 0 )( 5 . 0 ( ) 224 . 0 )( 5 . 0 ( = + = ºåi
i i w yw Z = Z 0 +wZ1 = 0.736
( ) ( ) = =196.7 cm
1.762
mol
V ZRT
P
3
H é
0 1
ù
( ) ( ) = +
w = -
1.029
ú úû
ê êë
R
pc
R
pc
R
pc
H
RT
H
RT
RT
é
= +
0 1
= -
ù
ú úû
S R R R
ê êë
S
R
S
R
R
w
H R = -4937 J /mol S R = -8.56 J /mol ×K