Page 1
Availability and Irreversibility
The sources of energy can be divided into two groups i.e., high grade energy
(mechanical work, electrical energy, water power, wind power) and low grade
energy (heat or thermal energy, heat derived from nuclear fission or combustion of
fossil fuels). That part of the low grade energy which is available for, conversion is
referred to as available energy, while the part which is not available is known as
unavailable energy.
Availability: When a system is subjected to a process from its original state to dead
state the maximum amount of useful work that can be achieved under ideal
conditions is known as available energy or availability of the system.
W m ax = AE = Q X y To(Sy-Sx)
Unavailable Energy:
UE = T0(Sy-Sx )
where, Sx and Sy are the entropy at x and y, respectively.
The Available Energy (AE) is also known as exergy and the Unavailable Energy (UE)
as energy.
Page 2
Availability and Irreversibility
The sources of energy can be divided into two groups i.e., high grade energy
(mechanical work, electrical energy, water power, wind power) and low grade
energy (heat or thermal energy, heat derived from nuclear fission or combustion of
fossil fuels). That part of the low grade energy which is available for, conversion is
referred to as available energy, while the part which is not available is known as
unavailable energy.
Availability: When a system is subjected to a process from its original state to dead
state the maximum amount of useful work that can be achieved under ideal
conditions is known as available energy or availability of the system.
W m ax = AE = Q X y To(Sy-Sx)
Unavailable Energy:
UE = T0(Sy-Sx )
where, Sx and Sy are the entropy at x and y, respectively.
The Available Energy (AE) is also known as exergy and the Unavailable Energy (UE)
as energy.
Available Energy from a Finite Energy Source: Consider a hot gas of mass m„ at
o o
temperature T when the environmental temperature is To. Assume that gas is
cooled from state 1 to state 3 and heat given by the gas Qi be utilized in heating up
reversibly a working fluid of mass mW f from state 3 to state 1. The working fluid
expands reversibly and adiabatically in an engine or turbine from state 1 to state 2
and then return to state 3 to complete heat engine cycle.
Available energy of a finite energy source
Available energy = W m a x = Q 1-Q 2
= C „ (T - T 0)-T.m „ C ,, In —
= »U Cp. (T -T 0)-T , I n -
Law of Degradation of Energy
First law states that energy is always conserved quantity wise while second law
emphasizes that energy always degrades quality wise. Second law is called the law
of degradation of energy. Energy is always conserved but its quality is always
degraded.
all the energy all the energy the gain in the gain in
that enters = that leaves + reversible + irreversible
the system the system energy enerav
L
Reversible work by an open system exchanging heat only with the surroundings.
, . v~ , F.:
dTT^ = dm ,
\ ~ ^ gZ.
— dm. h, — TtS2 gZ2
-d
J?IV"
U~T,S-\----- + mgZ
Where, Z\ and Z2 are the elevation at 1 and 2, respectively.
For steady flow process, = > dm7 =dm2 dm
dEv=0
The maximum reversible work
. r,:
~T-S: — y - y Z ,
The expression is called Kennan function B. In term of per unit mass is called
Kennan function 8.
Page 3
Availability and Irreversibility
The sources of energy can be divided into two groups i.e., high grade energy
(mechanical work, electrical energy, water power, wind power) and low grade
energy (heat or thermal energy, heat derived from nuclear fission or combustion of
fossil fuels). That part of the low grade energy which is available for, conversion is
referred to as available energy, while the part which is not available is known as
unavailable energy.
Availability: When a system is subjected to a process from its original state to dead
state the maximum amount of useful work that can be achieved under ideal
conditions is known as available energy or availability of the system.
W m ax = AE = Q X y To(Sy-Sx)
Unavailable Energy:
UE = T0(Sy-Sx )
where, Sx and Sy are the entropy at x and y, respectively.
The Available Energy (AE) is also known as exergy and the Unavailable Energy (UE)
as energy.
Available Energy from a Finite Energy Source: Consider a hot gas of mass m„ at
o o
temperature T when the environmental temperature is To. Assume that gas is
cooled from state 1 to state 3 and heat given by the gas Qi be utilized in heating up
reversibly a working fluid of mass mW f from state 3 to state 1. The working fluid
expands reversibly and adiabatically in an engine or turbine from state 1 to state 2
and then return to state 3 to complete heat engine cycle.
Available energy of a finite energy source
Available energy = W m a x = Q 1-Q 2
= C „ (T - T 0)-T.m „ C ,, In —
= »U Cp. (T -T 0)-T , I n -
Law of Degradation of Energy
First law states that energy is always conserved quantity wise while second law
emphasizes that energy always degrades quality wise. Second law is called the law
of degradation of energy. Energy is always conserved but its quality is always
degraded.
all the energy all the energy the gain in the gain in
that enters = that leaves + reversible + irreversible
the system the system energy enerav
L
Reversible work by an open system exchanging heat only with the surroundings.
, . v~ , F.:
dTT^ = dm ,
\ ~ ^ gZ.
— dm. h, — TtS2 gZ2
-d
J?IV"
U~T,S-\----- + mgZ
Where, Z\ and Z2 are the elevation at 1 and 2, respectively.
For steady flow process, = > dm7 =dm2 dm
dEv=0
The maximum reversible work
. r,:
~T-S: — y - y Z ,
The expression is called Kennan function B. In term of per unit mass is called
Kennan function 8.
IT'
I, w\r , , *«v: _
= ft--- ^-+mgZl - ft--- — - mgZ:
= W - V2
Where, V7 is called the availability function of a steady flow process given by
, , m\' , „
J J = O --------r msZ
If AKE = 0 and APE = 0
Wm ax = bi -b2 = (f> 1 - f> 2)"fo(Sl-S2)
Maximum reversible work for a closed system,
dm i = dm2 = 0
d it; - d U
T <- , f f l V ~ , 7
T r.S T — — + fflgZ
where, at
AKE=0, APE=0 Wm ax = (Ur T0Si)-(U2-T0S2)e
where, A KE = Change in kinetic energy
A PE = Change in potential energy
Maximum reversible work for unit mass of fluid,
Wmax = (U v T 0S M U 2-T 0S 2)
Useful Work
Maximum useful work Wm ax=Wm ax-po(l/2-^i)
Vi and V2 are the initial and final volumes of the systems and po is the atmospheric
pressure.
Useful Work for Unsteady Open System
f i
V-
dWv )-dmx\ hi~TtS i + ~ + gZl ¦-dm, \ k:- T.S, h —^-+gZ2
- d
rri V
L’ + p.V-T:S +——+ mgZ
Useful Work for Unsteady Closed System
[Vrr) = -d U+pJ'-TS + ^ - + mgZ
= - d [E +PiV — I S ]
i X ’ U = £ , - £ :+ P o (Ii-K )-r0(Si-S,)
AKE=0, APE=0
(Wu )m ax = Ui-U2+p0(Vi-V2)-T0(Si-S2)
(Wu )m ax = (Ui+p0V-T0Si)-(U2+p0V2-T0S2)
(Wu ) m ax = < p r< p 2 < | ) is called the availability function for a closed system,
(p = U + p0V -p0S
or q > = u + p0V - p0S (per unit mass basis)
Maximum useful work obtainable when the systems exchange heat with thermal
reservoirs in addition to the atmosphere
Page 4
Availability and Irreversibility
The sources of energy can be divided into two groups i.e., high grade energy
(mechanical work, electrical energy, water power, wind power) and low grade
energy (heat or thermal energy, heat derived from nuclear fission or combustion of
fossil fuels). That part of the low grade energy which is available for, conversion is
referred to as available energy, while the part which is not available is known as
unavailable energy.
Availability: When a system is subjected to a process from its original state to dead
state the maximum amount of useful work that can be achieved under ideal
conditions is known as available energy or availability of the system.
W m ax = AE = Q X y To(Sy-Sx)
Unavailable Energy:
UE = T0(Sy-Sx )
where, Sx and Sy are the entropy at x and y, respectively.
The Available Energy (AE) is also known as exergy and the Unavailable Energy (UE)
as energy.
Available Energy from a Finite Energy Source: Consider a hot gas of mass m„ at
o o
temperature T when the environmental temperature is To. Assume that gas is
cooled from state 1 to state 3 and heat given by the gas Qi be utilized in heating up
reversibly a working fluid of mass mW f from state 3 to state 1. The working fluid
expands reversibly and adiabatically in an engine or turbine from state 1 to state 2
and then return to state 3 to complete heat engine cycle.
Available energy of a finite energy source
Available energy = W m a x = Q 1-Q 2
= C „ (T - T 0)-T.m „ C ,, In —
= »U Cp. (T -T 0)-T , I n -
Law of Degradation of Energy
First law states that energy is always conserved quantity wise while second law
emphasizes that energy always degrades quality wise. Second law is called the law
of degradation of energy. Energy is always conserved but its quality is always
degraded.
all the energy all the energy the gain in the gain in
that enters = that leaves + reversible + irreversible
the system the system energy enerav
L
Reversible work by an open system exchanging heat only with the surroundings.
, . v~ , F.:
dTT^ = dm ,
\ ~ ^ gZ.
— dm. h, — TtS2 gZ2
-d
J?IV"
U~T,S-\----- + mgZ
Where, Z\ and Z2 are the elevation at 1 and 2, respectively.
For steady flow process, = > dm7 =dm2 dm
dEv=0
The maximum reversible work
. r,:
~T-S: — y - y Z ,
The expression is called Kennan function B. In term of per unit mass is called
Kennan function 8.
IT'
I, w\r , , *«v: _
= ft--- ^-+mgZl - ft--- — - mgZ:
= W - V2
Where, V7 is called the availability function of a steady flow process given by
, , m\' , „
J J = O --------r msZ
If AKE = 0 and APE = 0
Wm ax = bi -b2 = (f> 1 - f> 2)"fo(Sl-S2)
Maximum reversible work for a closed system,
dm i = dm2 = 0
d it; - d U
T <- , f f l V ~ , 7
T r.S T — — + fflgZ
where, at
AKE=0, APE=0 Wm ax = (Ur T0Si)-(U2-T0S2)e
where, A KE = Change in kinetic energy
A PE = Change in potential energy
Maximum reversible work for unit mass of fluid,
Wmax = (U v T 0S M U 2-T 0S 2)
Useful Work
Maximum useful work Wm ax=Wm ax-po(l/2-^i)
Vi and V2 are the initial and final volumes of the systems and po is the atmospheric
pressure.
Useful Work for Unsteady Open System
f i
V-
dWv )-dmx\ hi~TtS i + ~ + gZl ¦-dm, \ k:- T.S, h —^-+gZ2
- d
rri V
L’ + p.V-T:S +——+ mgZ
Useful Work for Unsteady Closed System
[Vrr) = -d U+pJ'-TS + ^ - + mgZ
= - d [E +PiV — I S ]
i X ’ U = £ , - £ :+ P o (Ii-K )-r0(Si-S,)
AKE=0, APE=0
(Wu )m ax = Ui-U2+p0(Vi-V2)-T0(Si-S2)
(Wu )m ax = (Ui+p0V-T0Si)-(U2+p0V2-T0S2)
(Wu ) m ax = < p r< p 2 < | ) is called the availability function for a closed system,
(p = U + p0V -p0S
or q > = u + p0V - p0S (per unit mass basis)
Maximum useful work obtainable when the systems exchange heat with thermal
reservoirs in addition to the atmosphere
h, -T,S. — mgZ,
mvz
U — T:S 4— ------mgZ 1 - i
Tx
TE — Temperature of resen'oir
Q_ — Heat received bv system
Dead State: When the system is in equilibrium with surrounding with temperature
To and pressure po and the system also in chemical equilibrium with zero velocity
and minimum potential energy. Then, it is called the dead state. All spontaneous
processes terminate at the dead state.
Irreversibility
The actual work done by a system is always less than idealized reversible work and
the difference between the two is called the irreversibility of the process.
l = Wmax-W
I = To(ASS ystem + ASsu rro u n cjin g)
/ = To(AS)universal
7o(AS)universai represent an increase in unavailable energy.
Goby-Stodola Theorem: It states that the rate of loss of available energy or exergy
in a process is proportional to the rate of entropy generation Sg en
I = W|ost = ToASuniversa|
/ = T o S g en
Insulation
© / ©
• ¦ - > ' v l- • • 4
* i
» * *
---- !-^ ----{-?
I t
W . - 7 / ¦ / / , S'/V/i A > V A ' - Z ’ .V A V / Z V / S / / /
Goby-Stodola theorem
where, / = irreversibility
Irreversibility for adiabatic flow of an ideal gas through the segment of pipe with
friction decreases in availability and is proportional to pressure drop and mass flow
rate.
I = = T.St(. - / = mRT, r E
ft
• The term Kennan function B(=H-ToS) is used in steady flow process and
availability function is given by
mgZ
• For closed system availability function is given by
= U + p cV — PrS
Page 5
Availability and Irreversibility
The sources of energy can be divided into two groups i.e., high grade energy
(mechanical work, electrical energy, water power, wind power) and low grade
energy (heat or thermal energy, heat derived from nuclear fission or combustion of
fossil fuels). That part of the low grade energy which is available for, conversion is
referred to as available energy, while the part which is not available is known as
unavailable energy.
Availability: When a system is subjected to a process from its original state to dead
state the maximum amount of useful work that can be achieved under ideal
conditions is known as available energy or availability of the system.
W m ax = AE = Q X y To(Sy-Sx)
Unavailable Energy:
UE = T0(Sy-Sx )
where, Sx and Sy are the entropy at x and y, respectively.
The Available Energy (AE) is also known as exergy and the Unavailable Energy (UE)
as energy.
Available Energy from a Finite Energy Source: Consider a hot gas of mass m„ at
o o
temperature T when the environmental temperature is To. Assume that gas is
cooled from state 1 to state 3 and heat given by the gas Qi be utilized in heating up
reversibly a working fluid of mass mW f from state 3 to state 1. The working fluid
expands reversibly and adiabatically in an engine or turbine from state 1 to state 2
and then return to state 3 to complete heat engine cycle.
Available energy of a finite energy source
Available energy = W m a x = Q 1-Q 2
= C „ (T - T 0)-T.m „ C ,, In —
= »U Cp. (T -T 0)-T , I n -
Law of Degradation of Energy
First law states that energy is always conserved quantity wise while second law
emphasizes that energy always degrades quality wise. Second law is called the law
of degradation of energy. Energy is always conserved but its quality is always
degraded.
all the energy all the energy the gain in the gain in
that enters = that leaves + reversible + irreversible
the system the system energy enerav
L
Reversible work by an open system exchanging heat only with the surroundings.
, . v~ , F.:
dTT^ = dm ,
\ ~ ^ gZ.
— dm. h, — TtS2 gZ2
-d
J?IV"
U~T,S-\----- + mgZ
Where, Z\ and Z2 are the elevation at 1 and 2, respectively.
For steady flow process, = > dm7 =dm2 dm
dEv=0
The maximum reversible work
. r,:
~T-S: — y - y Z ,
The expression is called Kennan function B. In term of per unit mass is called
Kennan function 8.
IT'
I, w\r , , *«v: _
= ft--- ^-+mgZl - ft--- — - mgZ:
= W - V2
Where, V7 is called the availability function of a steady flow process given by
, , m\' , „
J J = O --------r msZ
If AKE = 0 and APE = 0
Wm ax = bi -b2 = (f> 1 - f> 2)"fo(Sl-S2)
Maximum reversible work for a closed system,
dm i = dm2 = 0
d it; - d U
T <- , f f l V ~ , 7
T r.S T — — + fflgZ
where, at
AKE=0, APE=0 Wm ax = (Ur T0Si)-(U2-T0S2)e
where, A KE = Change in kinetic energy
A PE = Change in potential energy
Maximum reversible work for unit mass of fluid,
Wmax = (U v T 0S M U 2-T 0S 2)
Useful Work
Maximum useful work Wm ax=Wm ax-po(l/2-^i)
Vi and V2 are the initial and final volumes of the systems and po is the atmospheric
pressure.
Useful Work for Unsteady Open System
f i
V-
dWv )-dmx\ hi~TtS i + ~ + gZl ¦-dm, \ k:- T.S, h —^-+gZ2
- d
rri V
L’ + p.V-T:S +——+ mgZ
Useful Work for Unsteady Closed System
[Vrr) = -d U+pJ'-TS + ^ - + mgZ
= - d [E +PiV — I S ]
i X ’ U = £ , - £ :+ P o (Ii-K )-r0(Si-S,)
AKE=0, APE=0
(Wu )m ax = Ui-U2+p0(Vi-V2)-T0(Si-S2)
(Wu )m ax = (Ui+p0V-T0Si)-(U2+p0V2-T0S2)
(Wu ) m ax = < p r< p 2 < | ) is called the availability function for a closed system,
(p = U + p0V -p0S
or q > = u + p0V - p0S (per unit mass basis)
Maximum useful work obtainable when the systems exchange heat with thermal
reservoirs in addition to the atmosphere
h, -T,S. — mgZ,
mvz
U — T:S 4— ------mgZ 1 - i
Tx
TE — Temperature of resen'oir
Q_ — Heat received bv system
Dead State: When the system is in equilibrium with surrounding with temperature
To and pressure po and the system also in chemical equilibrium with zero velocity
and minimum potential energy. Then, it is called the dead state. All spontaneous
processes terminate at the dead state.
Irreversibility
The actual work done by a system is always less than idealized reversible work and
the difference between the two is called the irreversibility of the process.
l = Wmax-W
I = To(ASS ystem + ASsu rro u n cjin g)
/ = To(AS)universal
7o(AS)universai represent an increase in unavailable energy.
Goby-Stodola Theorem: It states that the rate of loss of available energy or exergy
in a process is proportional to the rate of entropy generation Sg en
I = W|ost = ToASuniversa|
/ = T o S g en
Insulation
© / ©
• ¦ - > ' v l- • • 4
* i
» * *
---- !-^ ----{-?
I t
W . - 7 / ¦ / / , S'/V/i A > V A ' - Z ’ .V A V / Z V / S / / /
Goby-Stodola theorem
where, / = irreversibility
Irreversibility for adiabatic flow of an ideal gas through the segment of pipe with
friction decreases in availability and is proportional to pressure drop and mass flow
rate.
I = = T.St(. - / = mRT, r E
ft
• The term Kennan function B(=H-ToS) is used in steady flow process and
availability function is given by
mgZ
• For closed system availability function is given by
= U + p cV — PrS
and
a = 4 ~ § >
where
f = l \ + P c , V o - T 0S c
Property Helmholty function F-be defined by the relation F = U - TS
Given function G is defined as G=H-TS=U+pV-TS
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