Energy: Quantity & Quality
Exergy
                                                                                                           Energy has both quantity and quality.
                                                                                                           Quality of energy is its potential to produce useful work.
                    Dr. Md. Zahurul Haq,          Ph.D., CEA, FBSME, FIEB
                                                                                                           First Law of Thermodynamics:
                                                                                                           energy is conserved in all (non-nuclear) processes.
                                        Professor
                         Department of Mechanical Engineering                                              Second Law of Thermodynamics:
               Bangladesh University of Engineering & Technology (BUET)
                               Dhaka-1000, Bangladesh
                                                                                                           the quality of energy is reduced in all real processes.
                               http://zahurul.buet.ac.bd/                                            ⇒ During transformation and transfer, energy is both conserved and
                                                                                                       degraded.
                    ME 203: Engineering Thermodynamics                                                     Exergy provides a direct relationship between the thermodynamic
                    http://zahurul.buet.ac.bd/ME203/                                                       state of a system and its capability to do useful work.
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Datum Condition & Useful Work
                                                                       012
                                                                                                                                                   P > P0
Standard atmosphere:
                                                                       4567
P0 = 101.325 kPa, T0 = 298.15 K                                                                    T1097
 Species RH = 60% RH=100%
                                                    80          012           012          30                          012345
 N2         0.7662      0.7564
                                                      80                                 30                                              T1093
 O2         0.2055      0.2029                                          089                                      91 5
 CO2        0.0003      0.0003                                                                                                                                                                                                                    
 H2 O       0.0188      0.0313                                                                                   1 5                                                                                                                        
                                                              55                55                                                                 P < P0
 Other      0.0092      0.0091                               657            657                                  0678
                                                   T1095               803                                        
  When the pressure, temperature, composition, velocity, or elevation of a                         T1096                 75               T1094
   system is different from the environment, there is an opportunity to
                                                                                                     Useful work could be produced by      Energy contains exergy when – and
                               develop work.
                                                                                                    utilizing temperature deviation from    only when – that energy is not in
                                                                                                               the environment.             equilibrium with its environment
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  Useful Work (Wu ) & Datum State (T0 , P0 )                                                    Dead State & Exergy (eX )
                                                                                                      A system in a dead state is in thermal & mechanical equilibrium
                                                                                                      with environment at T0 & P0 (T0 = 298.15 K, P0 = 101.325 kPa).
                                      P0                 Datum state                                  Exergy of a system in a closed system in a given state is the
              P                        F                 P0 = 101.325 kPa                             maximum useful work output that may be obtained from a
                                                         T0 = 298.15 K                                system-environment combination as the system proceeds from a
T345
                                                                                                      specified equilibrium state to the dead state, while exchanging
                               R2                                                                     heat solely with the environment.
           If P ≈ P0 ⇒ W =          PdV = P0 ∆V 6= 0;
                                1
                                                                                                      Exergy, eX ≡ Ex m is the sum of thermo-mechanical, KE, PE,
           −→But useful work, Wu = 0.                                                                 chemical exergies:
                 −
                 → →
           δWu = F .d −
                      x = (P − P0 )As dx = (P − P0 )dV = δW − P0 dV
                                                                                                                    eX = eXTM + eXKE + eXPE + eXCH + · · ·
       ⇒                δWu = δW − P0 dV = δW − δWsurr
                                                                                                      Exergy is a function of both the state of the system & the local
          As a closed system expands, some work needs to be done to push
                                                                                                      environment. Once the environmental conditions are standardized,
          the atmospheric air out of the way (and, vice versa)   Wsurr .
                                                                                                      exergy is treated as a property of the system alone.
         ⇒ Surrounding work (Wsurr ) is not recoverable & can’t be utilized.
                                                                                                      At dead state, exergy of the system is zero.
© Dr. Md. Zahurul Haq (BUET)              Exergy                   ME 203 (2022-23)   5 / 24   © Dr. Md. Zahurul Haq (BUET)          Exergy                   ME 203 (2022-23)   6 / 24
                                              Exergy Concepts: Examples                                                                  Exergy Concepts: Examples
                                                                                                Exergy of Heat (eXQ )
                                                                                               T341                           T487
                                                                                                                                  
                                                                                                                                T0
                                                                                                      ΦQ ≡ Wrev ,HE = Q 1 − T    R
 T1104                                       T1105
                                                                                                              Pn               
                                                                                                         ΦQ = j =0 Qj 1 − T   0
                                                                                                                             Tj
                                                                                                                       h          i
                                                                                                IQ = ΦQ,1 − ΦQ,2 = T0 Q T12 − T11 = T0 σQ
                                                                                                                                                      T1099
© Dr. Md. Zahurul Haq (BUET)              Exergy                   ME 203 (2022-23)   7 / 24   © Dr. Md. Zahurul Haq (BUET)          Exergy                   ME 203 (2022-23)   8 / 24
                                            Exergy Concepts: Examples                                                                        Exergy Concepts: Examples
                                                                                                Heat Conduction Through Wall
                                                                                                 Moran, Ex. 7-3 ⊲
                                                                                                                                                                  T2 −T1 
                                                                                                                                                       q̇ = −k      L  = 0.2 kW m2
T384                                        T385
                                                                                                                                                                  h       i
                                                                                                                                                                      T0
       ηcarnot = 1 − 300/1000 = 0.7                ηcarnot = 1 − 300/800 = 0.625                                                                       φ̇Q,in = q 1 − T 1
                                                                                                                                                                             = 0.1 kW
                                                                                                                                                                                   m2
       | W |= 1000(0.7) = 700 J                    | W |= 1000(0.625) = 625 J
                                                                                                                                                                   h        i
                                                                                                                                                       φ̇Q,out = q 1 − T
                                                                                                                                                                       T2 = 0.01 m 2
                                                                                                                                                                          0          kW
       | QL |= 1000 − 700 = 300 J                  | QL |= 1000 − 625 = 375 J
                                                                                                                                                                                         kW
                                                                                                                                                       IQ = φ̇Q,in − φ̇Q,out = 0.09      m2
  ⇒ Exergy destruction for heat transfer from 1000 K to 800 K, ExQ
  ⇒ ExQ = 1000(300)(1/800 − 1/1000) = 75 J
                                                                                              T1112
  ⇒ Reversible work loss = 700 J - 625 J = 75 J.
© Dr. Md. Zahurul Haq (BUET)          Exergy                     ME 203 (2022-23)    9 / 24    © Dr. Md. Zahurul Haq (BUET)              Exergy                   ME 203 (2022-23)   10 / 24
                                            Exergy Concepts: Examples                                                                        Exergy Concepts: Examples
Equations: CM & CV Systems                                                                      Example: Exergy of Air
 CM System:                                                                                           φ = (u − u0 ) + P0 (v − v0 ) − T0 (s − s0 )
       Q − W = ∆U                                                                                     u − u0 = cv (T − T0 )
       Wu = W − P0 ∆V = W − W0                                                                        v = RT
                                                                                                           P                                            
       φ = (u − u0 ) + P0 (v − v0 ) − T0 (s − s0 )                                                    s − s0 = cV ln TT0 + R ln vv0 = cP ln T       2
                                                                                                                                                      − R ln  P2
             P                                                                                                                                   T1         P1
       ΦQ = nj=1 Qj 1 − T     0
                             Tj                                                                       Environment: T0 = 298.15 K, P0 = 101.325 kPa.
       ∆Φ = ΦQ − Wu − Icm                                                                             ⊲   Air   at   298.15 K & 101.325 kPa: φ = 0 kJ/kg
 SSSF CV System:                                                                                      ⊲   Air   at   298.15 K & 50 kPa: φ = 27.4 kJ/kg
       Q − Wsf = m(∆h + ∆pe + ∆he) = m∆h                                                              ⊲   Air   at   298.15 K & 200 kPa: φ = 16.0 kJ/kg
                      ✯
                      ✟        0                                                                      ⊲   Air   at   200 K & 101.325 kPa: φ = 20.8 kJ/kg
       Wu = Wsf − P0✟✟
                    ∆V = Wsf
                                        2
                                                                                                      ⊲   Air   at   400 K & 101.325 kPa: φ = 14.4 kJ/kg
       ψ = (h − h0 ) − T0 (s − s0 ) + V2 + gz
             P                                                                                  When the pressure, temperature, composition, velocity, or elevation of a
       ΦQ = nj=1 Qj 1 − T     0
                             Tj                                                                    system is different from the environment, there is an opportunity to
                P              P                                                                                               develop work.
       ∆(mψ) = e ṁe ψe − i ṁi ψi = Φ̇Q − Ẇu − İcv
© Dr. Md. Zahurul Haq (BUET)          Exergy                     ME 203 (2022-23)   11 / 24    © Dr. Md. Zahurul Haq (BUET)              Exergy                   ME 203 (2022-23)   12 / 24
                                             Exergy Concepts: Examples                                                                      Exergy Concepts: Examples
CM System: Expansion of Steam inside Cylinder                                                  Evaluating the Exergy of Exhaust Gas
                                                                                                Moran Ex. 7.1 ⊲ A cylinder of an internal combustion engine contains
                                                                                                2450 cm3 of gaseous combustion products at a pressure of 7 bar and a
 Cengel, Ex. 8-11 ⊲ Piston-cylinder assembly contains 0.05 kg steam.                            temperature of 867oC just before the exhaust valve opens. Determine the
                                                                                                specific exergy of the gas, in kJ/kg. Assume, the combustion products as air
                                         Q − W = m(∆u + ∆KE + ∆PE ) ≃ m∆u
                                                                                                as ideal gas.
                                         φ ≡ (u − u0 ) + P0 (v − v0 ) − T0 (s − s0 )
                                         Wu = W −W0 = 8.826 −3.509 = 5.317 kJ                                                 T0 = 300 K, P0 = 1.0 bar
                                         φQ = 0: Heat loss to T0                                                              φ ≡ (u − u0 ) + P0 (v − v0 ) − T0 (s − s0 )
                                         ∆φ = −9.648 kJ                                                                       u − u0 = cv (T − T0 ) = 600 kJ/kg
                                         ICM = φQ − Wu − ∆φ = 4.331 kJ                                                        P0 (v − v0 ) = R( PP0 T − T0 ) = 39.36 kJ/kg
T1113
                                               Wu
                                         ǫ=   −∆φ    = 0.551                                                                  s −s0 = cp ln(T /T0 )−R ln(P/P0 ) = 0.7870 kJ/kg
                                                                                                                              φ = 324.54 kJ/kg
                                                                                               T1435
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                                             Exergy Concepts: Examples                                                                      Exergy Concepts: Examples
Second Law Efficiency (ηII ) or Effectiveness (ǫ)                                              Adiabatic Compression & Pumping
        A performance parameter based on the exergy concept is know as
        Second Law Efficiency (ηII ) or as Second Law Effectiveness (ǫ).
        A first-law efficiency gages how well the energy is used when                                  CM process:                               CV process:
        compared against an ideal process, whereas an effectiveness
                                                                                                       ∆Φ = ΦQ − Wu − Icm                        ∆Ψ = ΦQ − Wu − Icv
        indicates how well exergy is utilized.
                               useful exergy out         exergy destruction                            Wu = Wact + P0 ∆V                         Wu = Wact
                   ηII ≡ ǫ ≡       exergy in       =1−       exergy in                                      ∆Φ                                          ∆Ψ
                                                                                                       ǫ≡   Wact                                  ǫ≡    Wact
                                                                                                       Effectiveness (ǫ) is defined as the increase in the specific
                                                        Wout           12                              availability of the fluid per unit of actual work input.
                                              ηI =    QHT +QMT    = 25+50    = 16%
                                                                                                                                   Ws
                                                                    293                                First law efficiency, η ≡   Wact .                                                                         
                                              ExHT = 25        1 − 1098 = 18.33
                                                                   293                                                                        
                                              ExMT = 50        1 − 513     = 21.44
                                                         Wout
                                              ηII =   ExHT +ExMT    = 30.2%
T349
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                                                  Exergy Concepts: Examples                                                                          Exergy Concepts: Examples
Steam/Gas Turbine, Throttling & Nozzle                                                                    Heat Exchange without Mixing
                                                                    Turbines:
                                                                         wa
                                                                    η=   ∆h
                                                                    ∆ψ = φQ − wu − icv
                                                                             wa
                                                                    ǫ=       ∆ψ
                                                                                                           T476
T475
                                                                                                                  w = 0, q = 0, ∆ke = 0, ∆pe = 0
       Throttling:                                     Nozzle:                                                                            P         P
                                                         0                                                        SSSF Energy: 0 = 0 − 0 + i (mh)i − e (mh)e
               0
              w✟
           ✼− ✟
          q✓   ✯+ hi − he − ✘
                      0      ✘✘
                              ✿           0
                                                           w✟
                                                        ✓+ ✟
                                                       q✼   ✯=0
                                                                he − hi + ∆ke
       0 =✓                 ∆ke                        ✓                                                    ⇒ m1 h1 + m3 h3 = m1 h2 + m4 h4 → mc (h4 − h3 ) = −mh (h2 − h1 )
                      0                                        ∆kea
                                                       η=
               φQ✚
                 ❃− w✟
                    ✟✯
                                                                                                              Exergy balance:
                       0
       ∆ψ =    ✚     u − Icv                                   ∆kes
                                                                                                                                  0
                                                                                                                               W✟
                                                                                                                                ✯− I cv → m (ψ − ψ ) + m (ψ − ψ ) = −I
                                                                                                                                         0
                                                              ❃+ w✟
                                                                         0                                                 ✚❃− ✟
                                                             ✚                                                    ∆(mΨ) = ✚
                                                                 ✟✯
                                                                                   0                                      ΦQ               c  4   3     h  2   1      cv
                                                                  u − Icv
              ψe                                       ∆ψ = ✚
                                                            ΦQ
       ǫ=     ψi
                                                                                                                                  mc (ψ4 −ψ3 )                      mc ψ4 +mh ψ2
                                                        ǫ=     Ψe                                           ⇒               ǫ≡   −mh (ψ2 −ψ1 )      or        ǫ≡    mc ψ3 +mh ψ1
                                                               Ψi
                                                                                                                  The first form of ǫ for heat exchanger is usually preferred.
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                                                  Exergy Concepts: Examples                                                                          Exergy Concepts: Examples
SSSF Compressor                                                                                           Throttling Process
 Holman, Ex. 5.10: ⊲ A steady-flow compressor is used to compress air from
 1 bar, 25o C to 8 bar in an adiabatic process. The first-law efficiency, ηI , of
 the process is 87%. Calculate the irreversibility and ηII of the process if
                                                                                                           Cengel, P. 8-130 ⊲ Argon gas expands from 3.5 MPa and 100oC to 500 kPa in
 T0 = 293 K.
                                                                                                           an adiabatic expansion valve. For environment conditions of 100 kPa and
       Ψ ≡ (h − h0 ) − T0 (s − s0 ) +    V2        ∼ (h − h0 ) − T0 (s − s0 )
                                              + gz =                                                       25o C, determine (a) the exergy of argon at the inlet, (b) the exergy
                                          2
       wa = h1 − h2 = −cP (T2 − T1 ) : ws = h1 − h2s = −cP (T2s − T1 )                                     destruction during the process, and (c) the second-law efficiency.
               ws
       ηI =    wa   = 0.87                                                                                                                                         ψ1 = 223.8 kJ
                      (k −1)/k )                                                                                                                                 ψ2 = 103.3 kJ
                      P2                                  Wa
       T2s = T1       P1             = 540 K → T2a =      Cp   + T1 = 571 K
                                                                                                                                                                   Icv = −∆ψ = 120.5 kJ
       wa = −279.0 kJ/kg                                                                                  T1122
                                                                                                                                                                         ψ2
                                                                                                                                                                   ǫ=    ψ1   = 0.461
       wmin = −∆Ψ = −[(h2a − h1 ) − T0 (s2a − s1 )] = −259.8 kJ/kg
       isf = T0 (s2a − s1 ) = 19.2 kJ/kg
               ∆Ψ
       ηII =   wa    = 0.931 ◭
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                                                  Exergy Concepts: Examples                                                                                   Exergy Concepts: Examples
Nozzle                                                                                              Air Cooled Condenser
 Cengel, P. 8-71 ⊲ Hot combustion gases enter the nozzle of a turbojet engine.                       Cengel, P. 8-63 ⊲ Determine (a) the rate of heat rejected in the condenser, (b)
 Assuming the nozzle to be adiabatic and the surroundings to be at 20o C,                            the COP of this refrigeration cycle if the cooling load at these conditions is 6
 determine (a) the exit velocity and (b) the decrease in the exergy of the gases.                    kW, and (c) the rate of exergy destruction in the condenser.
 Take air properties for the combustion gases.
                                                p                                                                                                              QL = 6 kW
                                           V2 = V12 − ∆KE = 627 m/s
                                                                                                                                                               QH = ṁ(h2 − h1 ) = 9.98 kW
                                                   ψ1 = 368.9 kJ
                                                                                                                                                                          QL          QL
                                                                                                                                                               COP =      Win   =   QH −QL     = 1.5
                                                   ψ2 = 339.4 kJ
                                                                                                                                                               Icv = −∆ψ = 0.0998 kW
                                                   Icv − ∆ψ = 29.5 kJ
                                                                                                                                                                    ψe
                                                        ψ2                                                                                                     ǫ=   ψi   = 0.955
T1124                                              ǫ=   ψ1   = 0.92                                 T1116
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                                                  Exergy Concepts: Examples                                                                                   Exergy Concepts: Examples
SSSF Turbine                                                                                        Boiler
 Borgnakke, Ex. 8.5: ⊲                                                                               Borgnakke, Ex. 8.6: ⊲ Determine the second-law efficiency for this process
                                                                                                     and the irreversibility per kilogram of water evaporated. Assume, cp of the
                                                                                                     products of combustion is 1.155 kJ/kg K.
 T351
        Ψ ≡ (h − h0 ) − T0 (s − s0 ) +   V2        ∼ (h − h0 ) − T0 (s − s0 )
                                              + gz =
                                          2
        ẇs = ṁ1 h1 − ṁ2 h2s − ṁ3 h3s = 25.27 MW
                                                                                                    T1111                                                                              T1436
        ẇa = ṁ1 h1 − ṁ2 h2 − ṁ3 h3 = 20.18 MW                                                                        h            i
                                                                                                            mgas             h2 −h1
        ηI =    ẇa
                      = 0.799 ◭                                                                             mwater   =       h3 −h4       = 3.685 kg/kg
                ẇs
        ∆(ṁ Ψ) = ṁ1 Ψ1 − ṁ2 Ψ2 − ṁ3 Ψ3 = 24.65 MW                                                            mgas (ψ2 −ψ1 )
                                                                                                            ǫ=   mwater (ψ3 −ψ4 )          = 0.458
                   ẇa
        ηII =    ∆(ṁΨ)   = 0.819 ◭                                                                         Icv = −∆ψ = 9.09 kW
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