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Heat capacity = C
               = amount of heat the object receives for a
                1K temperature rise
               = does not depend on the mass
               = unit J K–1


  C      Heat it can take
                                           c =C
                                              m
   For 1 K temperature rise

Specific Heat capacity = c
              = amount of heat required to raise the
                temperature of 1 kg of object by 1K
              = depend on the mass
              = unit J kg–1 K–1
Subtance    Specific heat capacity
                (J kg–1 K–1)
Aluminium            910
 Copper              390
  Iron               470
 Mercury             138
   Ice              2000
 Water              4200
Molar Heat capacity = Cm
             = amount of heat required to raise the
               temperature of 1 mole of subtance by 1K
             = depend on the n
             = unit J mol–1 K–1                  Relative
                                           molecular/atomic mass

   C      Heat it can take
                                           Cm = mrc
                                                1000
   For 1 K temperature rise

Specific Heat capacity = c
              = amount of heat required to raise the
                temperature of 1 kg of object by 1K
              = depend on the mass
              = unit J kg–1 K–1
Subtance    Molar heat capacity
                (J mol–1 K–1)
Aluminium           24.6
 Copper             24.8
  Iron              26.3
 Mercury            27.7
   Ice              36.5
 Water              75.4
Q = C∆θ




Amount of heat
required to raise   Q = mc∆θ
the temperature




                    Q = nCm∆θ
F = pA

               A                dW = F dy                dV

                                dW = pA dy
Pressure = p                F
                                   = p dV

                   dy           ∫ dW = ∫     p dV
      heating
                                             V2
     Container and piston         W=     ∫        p dV
                                             V1
V2          expansion
                         W=   ∫        p dV     V2 > V 1
                                  V1
                                              ln V2 = +ve
Boyle’s law                                      V1
                           Constant              W = +ve
 P∝ 1
      V                    pressure
 P= k                              V2
                                              compression
                         W=p∫           dV
     V                                          V2 < V 1
                                   V1 V2
          V2 k
W=    ∫            dV      = p[ V ]           ln V2 = –ve
               V                        V1       V1
          V1
          V2 1            = p[V2 – V1]            W = –ve
= k   ∫        V
                    dV
          V1              = p∆V                V not change
                   V2                            V2 = V 1
= k [ ln V ]
                   V1                          ln V2 = ln 1 = 0
                                  V2              V1
= k [ln V2 – ln V1]      = k ln
                                  V1              W=0
V2          expansion
                W=   ∫        p dV     V2 > V 1
expansion                V1
 V2 > V 1                            ln V2 = +ve
                                        V1
 W = +ve          Constant              W = +ve
                  pressure
                          V2
                                     compression
                W=p∫           dV
                          V1 V2        V2 < V 1
                   = p[ V ]          ln V2 = –ve
                               V1       V1
compression      = p[V2 – V1]            W = –ve
 V2 < V 1         = p∆V               V not change
W = –ve                                 V2 = V 1
                                      ln V2 = ln 1 = 0
                         V2              V1
              W = k ln
                         V1              W=0
P
    Work done by gas
         expanding




0   V1    V2         V

P
    Work done on gas
      compressed




0   V2    V1         V
Reflects the principle of conservation of energy




   ∆Q = ∆U + W                     ∆Q = ∆U – W

  Heat     Increase    Work                      Work
 energy        in       done                      done
supplied    internal   by the                    on the
            energy       gas                       gas
+ve       –ve                  –ve
 Heat      Heat
                    +ve
                  Increase    Decrease
supplied   loss                    in
                      in
                   internal    internal
                    energy      energy
Example :
                                T      V


      820 cm3                   1000 cm3



                               P = 2 x 105 Pa

    Heat = 220 J         a) Work done by the gas ?
                         b) Change in internal energy ?
  Solution :
                          V2
a) P constant      W=p∫        dV   = p ∆V
                          V1
                   = (2 x 105)[(1000 x (10–2)3) – 820 x (10–2)3]
                   = + 36 J
b) ∆Q = ∆U + W
                             +ve means
   ∆U = ∆Q – W = 220 – 36    internal energy
                             increases
                 = + 184 J
KE      Always in motion
Molecules have
                 PE      Forces of attraction
                         between molecules

 ∆Q = ∆U + W             ∆Q = ∆U + W
                 ∆U
                          ∆U = ∆Q – W
heating
                         When work done on gas,
  ∆Q                     W = –ve
                 Case     ∆U = ∆Q – ( – W)
  KE
                 where         = ∆Q + W
  ∆U             ∆U 
                                ∆U is +ve
Conclusion :
                       By heating
           ∆U 
                      Performing mechanical work on gas



 ∆Q = ∆U + W                   ∆Q = ∆U + W
                    ∆U
                                ∆U = ∆Q – W
heating
                               When work done on gas,
  ∆Q                           W = –ve
                   Case         ∆U = ∆Q – ( – W)
  KE
                   where            = ∆Q + W
  ∆U               ∆U 
                                    ∆U is +ve
For ideal gas :
No force of attraction                the separation is large



                         No PE involve,
                         Only KE involves

 From
 Molecular KE                                       T constant
                             KE ∝ T
 = 3/2 KT                                           ∆U = 0



                             ∆U ∝ T
Heat supplied to increase the temperature of n moles of gas
by 1K at constant pressure :

                   ∆Q = nCp,m ∆T

           Molar heat capacity at constant pressure


Heat supplied to increase the temperature of n moles of gas
by 1K at constant volume :
                   ∆Q = nCV,m ∆T

            Molar heat capacity at constant volume
Change of state of one mole of an ideal gas




    Case 1                              Case 2




p              p + ∆p            p                  p
V              V                 V                  V + ∆V
T              T + ∆T            T                  T + ∆T
Work done by a gas :
                   W = p∆V

                      = p(0)

                      =0




                ∆Q = ∆U + W
∆Q = CV,m∆T     CV,m∆T = ∆U + 0
                ∆U = CV,m∆T
Work done by a gas :
                           W = p∆V = R∆T


                 pVm = RT --(1)

                     p(Vm + ∆V) = R(T + ∆T)
                     pVm + p∆V) = RT + R∆T --(2)

                (2) – (1) : p∆V = R∆T
  ∆Q = Cp,m∆T
                   ∆Q = ∆U + W

From case 1 :   Cp,m∆T = CV,m∆T + R∆T

∆U = CV,m∆T       Cp,m = CV,m + R
                  Cp,m – CV,m = R
Cp,m – CV,m = R


   Cp.m > CV,m
p
              Case 1 (isochoric process)
p + ∆p         Case 2 (isobaric process)



     p



                        V
    0    Vm   Vm + ∆V
γ
        Cp,m
γ   =          Ratio of principal molar heat capacities
        CV,m


Cp,m and CV,m depend on the degrees of freedom
f
One mole of ideal gas has internal energy :   U=   RT
                                                 2
                    ∆Q = ∆U + W

∆Q = CV,m∆T         CV,m∆T = ∆U            W = p∆V = p(0) = 0

                    CV,m = ∆U
                             ∆T
  As ∆T  0         CV,m = dU
                             dT
                           f                     It is shown
                          = R
                           2                     that Cp,m
                                   f             and CV,m
Cp,m – CV,m = R         Cp,m   = R+ R
                                   2
                                                 depend on
                                   f+2           degrees of
                               =       R
                                    2            freedom
Cp,m
                                  γ   =          =
                                          CV,m

                                                 = f +2
                                                     f
For monoatomic : f = 3
                 γ = 3+2 = 1.67
                       3
                          For polyatomic : f = 6
For diatomic : f = 5                       γ = 6+2 = 1.33
               γ = 5+2 = 1.4                     6
                     5
Constant temperature           pV = constant

                               Boyle’s law

                           p
Internal energy constant               T1 < T2 < T3
      ∆U = 0                                 isotherm

                                                  T3
                                             T2
                                         T1

                           0                           V
Isothermal compression      Isothermal expansion


               Work                         Work
               done on                      done by
               gas                          gas

               T constant                   T constant
Heat escapes                  Heat enters
Vf
pV = nRT   W=∫        p dV
                 Vi                  p
                 Vf
p = nRT     =∫     nRT dV
                                                Isothermal
     V           Vi V                pi
                        Vf 1
                                                expansion
            = nRT ∫          V dV    pf
                        Vi
 Work                          Vf
 Done       = nRT [ ln V ]            0    Vi   Vf           V
  By                           Vi
 Ideal
  gas       = nRT [ln Vf – ln Vi]

            = nRT ln Vf             W = +ve  Vf > Vi
                     Vi
W = nRT ln Vf
                                    Vi
piVi = pfVf          piVi ln Vf = pfVf ln Vf      pV = nRT
                             Vi           Vi

First law of thermodynamic : ∆Q = ∆U + W

                            ∆Q = W             ∆U = 0
Work done on the gas
Vf
pV = nRT   W=∫        p dV
                 Vi                  p
                 Vf
p = nRT     =∫     nRT dV
                                                Isothermal
     V           Vi V                pf
                        Vf 1
                                                compression
            = nRT ∫          V dV    pi
                        Vi
 Work                          Vf
 Done       = nRT [ ln V ]            0    Vf   Vi       V
  on                           Vi
 Ideal
  gas       = nRT [ln Vf – ln Vi]

            = nRT ln Vf             W = –ve  Vf < Vi
                     Vi

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Thermodynamics of gases1

  • 1.
  • 2.
  • 3. Heat capacity = C = amount of heat the object receives for a 1K temperature rise = does not depend on the mass = unit J K–1 C Heat it can take c =C m For 1 K temperature rise Specific Heat capacity = c = amount of heat required to raise the temperature of 1 kg of object by 1K = depend on the mass = unit J kg–1 K–1
  • 4. Subtance Specific heat capacity (J kg–1 K–1) Aluminium 910 Copper 390 Iron 470 Mercury 138 Ice 2000 Water 4200
  • 5. Molar Heat capacity = Cm = amount of heat required to raise the temperature of 1 mole of subtance by 1K = depend on the n = unit J mol–1 K–1 Relative molecular/atomic mass C Heat it can take Cm = mrc 1000 For 1 K temperature rise Specific Heat capacity = c = amount of heat required to raise the temperature of 1 kg of object by 1K = depend on the mass = unit J kg–1 K–1
  • 6. Subtance Molar heat capacity (J mol–1 K–1) Aluminium 24.6 Copper 24.8 Iron 26.3 Mercury 27.7 Ice 36.5 Water 75.4
  • 7. Q = C∆θ Amount of heat required to raise Q = mc∆θ the temperature Q = nCm∆θ
  • 8. F = pA A dW = F dy dV dW = pA dy Pressure = p F = p dV dy ∫ dW = ∫ p dV heating V2 Container and piston W= ∫ p dV V1
  • 9. V2 expansion W= ∫ p dV V2 > V 1 V1 ln V2 = +ve Boyle’s law V1 Constant W = +ve P∝ 1 V pressure P= k V2 compression W=p∫ dV V V2 < V 1 V1 V2 V2 k W= ∫ dV = p[ V ] ln V2 = –ve V V1 V1 V1 V2 1 = p[V2 – V1] W = –ve = k ∫ V dV V1 = p∆V V not change V2 V2 = V 1 = k [ ln V ] V1 ln V2 = ln 1 = 0 V2 V1 = k [ln V2 – ln V1] = k ln V1 W=0
  • 10. V2 expansion W= ∫ p dV V2 > V 1 expansion V1 V2 > V 1 ln V2 = +ve V1 W = +ve Constant W = +ve pressure V2 compression W=p∫ dV V1 V2 V2 < V 1 = p[ V ] ln V2 = –ve V1 V1 compression = p[V2 – V1] W = –ve V2 < V 1 = p∆V V not change W = –ve V2 = V 1 ln V2 = ln 1 = 0 V2 V1 W = k ln V1 W=0
  • 11. P Work done by gas expanding 0 V1 V2 V P Work done on gas compressed 0 V2 V1 V
  • 12. Reflects the principle of conservation of energy ∆Q = ∆U + W ∆Q = ∆U – W Heat Increase Work Work energy in done done supplied internal by the on the energy gas gas
  • 13. +ve –ve –ve Heat Heat +ve Increase Decrease supplied loss in in internal internal energy energy
  • 14. Example : T V 820 cm3 1000 cm3 P = 2 x 105 Pa Heat = 220 J a) Work done by the gas ? b) Change in internal energy ? Solution : V2 a) P constant W=p∫ dV = p ∆V V1 = (2 x 105)[(1000 x (10–2)3) – 820 x (10–2)3] = + 36 J
  • 15. b) ∆Q = ∆U + W +ve means ∆U = ∆Q – W = 220 – 36 internal energy increases = + 184 J
  • 16.
  • 17. KE Always in motion Molecules have PE Forces of attraction between molecules ∆Q = ∆U + W ∆Q = ∆U + W ∆U ∆U = ∆Q – W heating When work done on gas, ∆Q W = –ve Case ∆U = ∆Q – ( – W) KE where = ∆Q + W ∆U ∆U  ∆U is +ve
  • 18. Conclusion : By heating ∆U  Performing mechanical work on gas ∆Q = ∆U + W ∆Q = ∆U + W ∆U ∆U = ∆Q – W heating When work done on gas, ∆Q W = –ve Case ∆U = ∆Q – ( – W) KE where = ∆Q + W ∆U ∆U  ∆U is +ve
  • 19. For ideal gas : No force of attraction the separation is large No PE involve, Only KE involves From Molecular KE T constant KE ∝ T = 3/2 KT ∆U = 0 ∆U ∝ T
  • 20.
  • 21. Heat supplied to increase the temperature of n moles of gas by 1K at constant pressure : ∆Q = nCp,m ∆T Molar heat capacity at constant pressure Heat supplied to increase the temperature of n moles of gas by 1K at constant volume : ∆Q = nCV,m ∆T Molar heat capacity at constant volume
  • 22.
  • 23.
  • 24. Change of state of one mole of an ideal gas Case 1 Case 2 p p + ∆p p p V V V V + ∆V T T + ∆T T T + ∆T
  • 25. Work done by a gas : W = p∆V = p(0) =0 ∆Q = ∆U + W ∆Q = CV,m∆T CV,m∆T = ∆U + 0 ∆U = CV,m∆T
  • 26. Work done by a gas : W = p∆V = R∆T pVm = RT --(1) p(Vm + ∆V) = R(T + ∆T) pVm + p∆V) = RT + R∆T --(2) (2) – (1) : p∆V = R∆T ∆Q = Cp,m∆T ∆Q = ∆U + W From case 1 : Cp,m∆T = CV,m∆T + R∆T ∆U = CV,m∆T Cp,m = CV,m + R Cp,m – CV,m = R
  • 27. Cp,m – CV,m = R Cp.m > CV,m
  • 28. p Case 1 (isochoric process) p + ∆p Case 2 (isobaric process) p V 0 Vm Vm + ∆V
  • 29. γ Cp,m γ = Ratio of principal molar heat capacities CV,m Cp,m and CV,m depend on the degrees of freedom
  • 30. f One mole of ideal gas has internal energy : U= RT 2 ∆Q = ∆U + W ∆Q = CV,m∆T CV,m∆T = ∆U W = p∆V = p(0) = 0 CV,m = ∆U ∆T As ∆T  0 CV,m = dU dT f It is shown = R 2 that Cp,m f and CV,m Cp,m – CV,m = R Cp,m = R+ R 2 depend on f+2 degrees of = R 2 freedom
  • 31. Cp,m γ = = CV,m = f +2 f For monoatomic : f = 3 γ = 3+2 = 1.67 3 For polyatomic : f = 6 For diatomic : f = 5 γ = 6+2 = 1.33 γ = 5+2 = 1.4 6 5
  • 32.
  • 33. Constant temperature pV = constant Boyle’s law p Internal energy constant T1 < T2 < T3 ∆U = 0 isotherm T3 T2 T1 0 V
  • 34. Isothermal compression Isothermal expansion Work Work done on done by gas gas T constant T constant Heat escapes Heat enters
  • 35. Vf pV = nRT W=∫ p dV Vi p Vf p = nRT =∫ nRT dV Isothermal V Vi V pi Vf 1 expansion = nRT ∫ V dV pf Vi Work Vf Done = nRT [ ln V ] 0 Vi Vf V By Vi Ideal gas = nRT [ln Vf – ln Vi] = nRT ln Vf W = +ve  Vf > Vi Vi
  • 36. W = nRT ln Vf Vi piVi = pfVf piVi ln Vf = pfVf ln Vf pV = nRT Vi Vi First law of thermodynamic : ∆Q = ∆U + W ∆Q = W ∆U = 0
  • 37. Work done on the gas
  • 38. Vf pV = nRT W=∫ p dV Vi p Vf p = nRT =∫ nRT dV Isothermal V Vi V pf Vf 1 compression = nRT ∫ V dV pi Vi Work Vf Done = nRT [ ln V ] 0 Vf Vi V on Vi Ideal gas = nRT [ln Vf – ln Vi] = nRT ln Vf W = –ve  Vf < Vi Vi