SF Prep
03 Chemistry Notes 🕒 Updated 2026-10-07
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Thermodynamic Systems & Boundaries

Thermodynamics

1. Thermodynamic Systems & Boundaries

  • System: Any macroscopic part of the universe that is under observation.
  • Surroundings: Apart from the system, everything else is the surroundings.
  • Universe = System + Surroundings.
  • Boundary: The wall that separates the system from its surroundings. It can be:
    • Real or Imaginary
    • Rigid or Non-Rigid: Rigid boundaries hold a constant volume. Non-rigid boundaries (e.g., fitted with a piston) can change volume.
    • Permeable or Impermeable: Permeable allows mass exchange; impermeable does not allow mass exchange.
    • Adiabatic or Diathermic: Adiabatic means heat flow is not allowed (q = 0). Diathermic means heat flow is allowed (q ≠ 0).

2. Types of Systems

System TypeHeat Exchange (q)Mass Exchange (Δm)Examples
Openq ≠ 0Δm ≠ 0Open container, animal/plant, pond, earth.
Closedq ≠ 0Δm = 0Container closed with a lid, closed container with piston.
Isolatedq = 0Δm = 0Universe, thermos flask.

3. Extensive & Intensive Properties

  • Extensive Properties: Properties whose value depends on the amount or size of the matter present in the system (i.e., changes on changing the amount of matter).
    • They are additive. (e.g., 5g + 5g = 10g mass).
    • Examples: Mass, Volume, Moles (n), and All energy terms (Internal Energy, Enthalpy, Kinetic Energy, Potential Energy, Entropy, Gibbs Free Energy, Total Energy).
  • Intensive Properties: Properties which do not depend on the amount or size of matter present.
    • They are non-additive.
    • If two identical systems are combined, their intensive properties do not add up (e.g., Molarity M₁ + M₂ is incorrect. Instead, Mnet = M₁V₁ + M₂V₂V₁ + V₂).

Key Rules for Intensive Properties:

  • The ratio of two extensive properties is an intensive property (e.g., Density = Mass / Volume).
  • If an extensive property is defined as "per mole", "per gram", "per liter", or "per ml", it becomes intensive. Thus, properties starting with "Molar" or "Specific" are intensive (e.g., Molar Mass, Molar Volume, Molar Heat Capacity, Molar Conductance, Specific Heat, Specific Volume, Specific Resistance).
  • Properties which do not change on the division of a system are intensive (e.g., Pressure P, Temperature T).
  • All concentration terms are intensive: Molarity, Molality, Normality, Formality, Mole fraction, Strength, Percentage and parts concentration terms.
  • All types of temperatures are intensive: Temperature, Boiling Point, Melting Point, Freezing Point.
  • All equilibrium constants are intensive: Kc, Kp, Kw, Kf, Ksp, Ka.

Algebraic Operations:

  • If X and Y are Extensive properties:
    X + Y = Ext,    X − Y = Ext,    X × Y = Ext,    X ÷ Y = Intensive.
  • If X and Y are Intensive properties:
    X + Y = Int,    X − Y = Int,    X × Y = Int,    X ÷ Y = Int.

4. State Functions vs Path Functions

  • State Function : Functions or variables whose value depends on the state of the system, not on the path adopted by the system to attain that state.
    Examples : Pressure (P), Volume (V), Temperature (T), Internal energy (U), Entropy (S), Enthalpy (H), Free energy (G).
  • Notation for changes in state variables: small changes = δU, δH, δG... ; large changes = ΔU, ΔH, ΔG...
  • Path Function : Quantities which are dependent on the path adopted by the system to achieve a particular state. These are defined when a process is going on.
    Examples : Work (W), Heat (q), Heat Capacity (C).
  • Notation for changes in path variables: small change = δq, δW ; large change = q, W.
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Thermodynamic Processes & Relation Between ΔH and ΔU for Gases

5. Thermodynamic Processes

  • Thermodynamic Process : Steps followed by the system to change its state (e.g., from State 1 (P₁, V₁, T₁) to State 2 (P₂, V₂, T₂)).
  • Isothermal Process : Temperature is constant (ΔT = 0, dT = 0).
    For an ideal gas : PV = constant ⇒ P₁V₁ = P₂V₂ (Boyle's Law).
  • Isochoric Process : Volume remains constant (ΔV = 0, dV = 0).
    For an ideal gas : P ∝ T ⇒ P₁/T₁ = P₂/T₂ (Gay Lussac's Law).
  • Isobaric Process : Pressure remains constant (ΔP = 0, dP = 0).
    For an ideal gas : V ∝ T ⇒ V₁/T₁ = V₂/T₂ (Charle's Law).
  • Adiabatic Process : Heat exchange is not allowed (q = 0, dq = 0).
    For an ideal gas : PVγ = constant (where γ = Poisson's ratio, γ > 1).
Isothermal : PV = constant  |  Adiabatic : PVγ = constant
VP A Isothermal Adiabatic Expansion VP A Isothermal Adiabatic Compression
  • Cyclic Process : When a system undergoes different states by different processes and finally returns to its initial state.
  • For a cyclic process, the change in all state functions is zero : ΔU = 0, ΔS = 0, ΔG = 0, ΔH = 0, ΔT = 0, ΔP = 0. Net heat (q) and net work (W) are not zero.

6. Internal Energy (U) & Enthalpy (H)

  • Internal Energy (U / E) : Every substance possesses a definite amount of energy depending on composition, temperature, and pressure.
    U = Ut + Ur + Uv + Ue + ... (translational, rotational, vibrational, electronic, etc.)
  • Since U is a state function, its absolute value cannot be determined, but its change can be: ΔU = U₂ − U₁.
  • Enthalpy (H) : Used when dealing with processes in open vessels (at constant pressure) instead of internal energy.
H = U + PV  ⇒  ΔH = ΔU + Δ(PV)
  • General relation between states 1 and 2 : ΔH = ΔU + (P₂V₂ − P₁V₁)

7. Relation Between ΔH and ΔU for Gases

  • From ideal gas law PV = nRT, taking changes gives Δ(PV) = ΔnRT + nRΔT.
  • For an ideal gas (only temperature changes, no chemical reaction) :
ΔH = ΔU + nRΔT
  • For a chemical reaction (at constant temperature) :
ΔH = ΔU + ΔngRT

Δng = (Moles of product gases) − (Moles of reactant gases)

  • If Δng = 0, then ΔH = ΔU. (e.g., C (s) + O₂ (g) → CO₂ (g)).

8. Heat (q)

  • Quantity of energy which flows between a system and its surroundings on account of a temperature difference. Heat always flows from high to low temperature.
  • IUPAC Sign Convention :
    • Heat flowing into the system : q = +ve
    • Heat flowing out of the system : q = −ve

9. Work & Heat

  • Heat and work are both dynamic forms of energy and are boundary phenomena.

Mathematical Expression of Work :

W = − ∫V₁V₂ Pext dV
  • Pext is the pressure which is used to compress the gas (contraction).
  • Pext is the pressure against which the gas is doing work (expansion).

Special Cases :

  • Case-1 (Pext = constant) :
    W = −Pext ∫ dV = −Pext(V₂ − V₁)
  • Case-2 (Pext ≠ constant) :
    W = − ∫ Pext dV

Sign Convention :

  • W is taken as negative if work is done by the system.
  • W is taken as positive if work is done on the system.
  • When heat is given by the system to the surrounding, it is given a negative sign (−q).
  • When heat is absorbed by the system from the surrounding, it is positive (+q).
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Zeroth Law of Thermodynamics

10. Zeroth Law of Thermodynamics

  • If two systems A and B are each in thermal equilibrium with a third system C, then A and B are in thermal equilibrium with each other.
  • Equivalently: if TA = TC and TB = TC, then TA = TB.

11. First Law of Thermodynamics (FLOT)

ΔU = q + W

U₂ = U₁ + q + W  ⇒  U₂ − U₁ = q + W

FLOT on Different Processes :

  • Isothermal Process (dT = 0, ΔT = 0) :
    ΔH = 0. For an ideal gas, ΔU = 0 (only when molecular interactions during the process remain the same).
    Since ΔU = q + W = 0 ⇒ +q = −W or −q = +W.
  • Exceptions (Isothermal but ΔU ≠ 0, ΔH ≠ 0) : Phase changes like Ice ⇌ water (at M.P.) and water ⇌ Vapour (at B.P.).
  • Adiabatic Process (q = 0) :
    ΔU = q + W ⇒ ΔU = W.
    → If work is done on the system, its internal energy increases (TFinal > Tinitial).
    → If work is done by the system, its internal energy decreases (TFinal < Tinitial).
  • Isochoric Process (dV = 0) :
    W = 0 ⇒ ΔU = qv.
    Heat supplied to the system or by the system is equal to the change in internal energy.
  • Isobaric Process (ΔP = 0) :
    ΔU = q + W ⇒ U₂ − U₁ = q − P(V₂ − V₁)
    (U₂ + PV₂) − (U₁ + PV₁) = qp ⇒ H₂ − H₁ = qp ⇒ ΔH = qp.
ΔH = ΔU + ΔngRT

12. Heat Capacity

  • Defined as the quantity of heat required to raise the temperature of the system by one degree.
  • Larger the sample, greater is its heat capacity.
C = dqdT

Unit is J K−1 or J / °C

Specific Heat Capacity (s) :

s = dqm dT   (J / g K or J / g °C)
  • Heat supplied to the system to raise its temp from T₁ to T₂ :
    q = m ∫ s dT. If specific heat capacity is given as constant, Q = ms(T₂ − T₁).

Molar Heat Capacity (C) :

C = dqn dT   (J / mol K)
  • q = n ∫ C dT. If C is constant, q = nC(T₂ − T₁).

13. Heat Capacity at Constant Pressure & Volume

  • For gaseous systems :
    Cp = molar heat capacity at constant pressure.
    Cv = molar heat capacity at constant volume.
  • At constant volume (W = 0) : qv = ΔE ⇒ Cv = (dE/dT)v per mole (or dU/dT).
  • At constant pressure : qp = ΔH ⇒ Cp = (dH/dT)p per mole.
Cp > Cv
  • Cp is "generally" larger than Cv because at constant pressure, a part of the heat added may be used in the work of expanding, whereas at constant volume all added heat produces a rise in temperature.
  • Exception : Substances generally expand with an increase of temperature at constant pressure, but there may be contraction in exceptional cases (e.g., water between 0° & 4°).

Relation between Cp and Cv :

For 1 mole of an ideal gas :

  • H = U + PV = U + RT
  • dHdT = dUdT + R
Cp − Cv = R

14. Molar Heat Capacities of Gases

GasCvCpPoisson's Ratio (γ)Example
Monoatomic32 R52 R1.67He, Ne, Ar
Diatomic52 R72 R1.40O2, N2, H2
Linear Polyatomic52 R72 R1.40CO2, HCN
Non-linear Polyatomic3 R4 R1.33CH4, H2O, NH3

γ = Cp/Cv (Poisson's ratio) ; Cp − Cv = R

  • For temperature-dependent specific heat, heat exchanged is calculated using integration : q = n ∫ C dT.

15. Mixture of Gases

  • For a mixture of non-reacting ideal gases, the effective molar heat capacities and Poisson's ratio (γmix) are :
Cv,mix = n₁Cv1 + n₂Cv2 + ...n₁ + n₂ + ...   ;   γmix = Cp,mixCv,mix
  • Since Cp,mix − Cv,mix = R, we know Cv = Rγ − 1. Substituting this into the mixture formula gives:
n₁ + n₂ + ...γmix − 1 = n₁γ₁ − 1 + n₂γ₂ − 1 + ...
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Reversible & Irreversible Processes

16. Reversible & Irreversible Processes

  • Reversible Process :
    • Completion time is infinite (hypothetical process).
    • Equilibrium is maintained in every step.
    • Both internal and external pressure change, but external pressure is always equal to internal pressure (Pext = Pgas).
    • If we reverse the process, each step is achieved back.
  • Irreversible Process :
    • Finite step process (all processes in nature are irreversible).
    • Fast process where external pressure is constant.
    • Equilibrium is not observed in between.
    • In the case of expansion processes, external pressure is much less than the internal pressure (Pext << Pgas).

17. Thermodynamic Changes in Isothermal Process

Reversible Isothermal Expansion (from V₁ to V₂) :

  • Here, Pext = Pgas (but is variable).
  • dW = −(Pext − dP) dV = −Pext dV + dP dV (where dP dV → 0)
  • ∫ dW = − ∫V₁V₂ Pext dV = − ∫V₁V₂ Pgas dV = − ∫V₁V₂ nRTV dV
Wrev = −nRT ln(V₂V₁) = −2.303 nRT log(V₂V₁)

Since P₁V₁ = P₂V₂, we can also write Wrev = −2.303 nRT log(P₁/P₂).

Irreversible Isothermal Expansion (from V₁ to V₂) :

  • Here, Pext is constant and Pext << Pgas.
  • ∫ dW = − ∫V₁V₂ Pext dV
Wirr = −Pext (V₂ − V₁)
  • Generally, the final pressure of the gas P₂ = Pext. Using PV = nRT (so P₁/P₂ = V₂/V₁):
Wirr = −P₂ (V₂ − V₁) = nRT (V₁V₂ − 1) = nRT (P₂P₁ − 1)

18. Work Done : Reversible vs Irreversible Process

  • Expansion (V₁ → V₂) :
    • Reversible : Gas expands against an external pressure almost equal to gas pressure (Pext = Pgas).
    • Irreversible : Gas expands against a pressure much less than the gas pressure (Pext << Pgas).
    • Magnitude of work done by gas : Wrev > Wirrev. Area under reversible curve is greater.
  • Compression :
    • Reversible : Gas is compressed by an external pressure equal to Pgas.
    • Irreversible : Gas is compressed by an external pressure much greater than Pgas (Pext >> Pgas).
    • Magnitude of work done on gas : Wirrev > Wrev. Area under irreversible path (rectangle) is greater.
Wirrev = −Pext(V₂ − V₁) = −P₂(V₂ − V₁) = nRTV₁V₂ − nRT = nRT(P₂P₁ − 1)
Expansion P₁P₂ V₁V₂ rev. irrev. Compression P₂P₁ V₂V₁ rev. irrev.

19. Free Expansion

  • Expansion of an ideal gas into a vacuum where Pext = 0.
W = 0  ,  q = 0  ,  ΔU = 0

20. Adiabatic Reversible Process

  • Conditions : Walls should be adiabatic ; heat exchange q = 0.
  • Expansion : Work is done by the system ⇒ Internal energy decreases (ΔU = negative) ⇒ Tfinal < Tinitial.
  • Compression : Work is done on the system ⇒ Internal energy increases (ΔU = positive) ⇒ Tfinal > Tinitial.
  • Derivation : ΔU = q + W ⇒ ΔU = W
    nCv dT = −Pgas dV = −(nRT/V) dV
    Cv (dT/T) = −R (dV/V)
    Integrating from T₁, V₁ to T₂, V₂ : ln(T₂/T₁) = −(γ−1) ln(V₂/V₁) ⇒ T₁V₁γ−1 = T₂V₂γ−1
  • Useful relations : Cp − Cv = R  ;  Cp/Cv = γ  ;  R/Cv = γ − 1
TVγ−1 = constant
PVγ = constant
P1−γ Tγ = constant  ⇒  T P(1−γ)/γ = constant

Derived by substituting P = nRT/V or V = nRT/P into the original equations.

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Adiabatic & Isothermal Expansion

21. Adiabatic & Isothermal Expansion

  • For reversible adiabatic processes, the following relations hold :
P1V1γ = P2V2γ   |   T1V1γ−1 = T2V2γ−1   |   T1P1(1−γ)/γ = T2P2(1−γ)/γ
  • From the First Law (ΔU = q + W), for an adiabatic process q = 0, therefore ΔU = W.
  • Work done (Reversible) : Since ΔU = nCv(T2 − T1) and P2V2 − P1V1 = nR(T2 − T1) :
W = nCv(T2 − T1) = nR(T2 − T1)γ − 1 = P2V2 − P1V1γ − 1
  • Work done (Irreversible) : Expanding against a constant external pressure Pext (where Pext = P2) :
nCv(T2 − T1) = −Pext(V2 − V1) = −P2(nRT2P2 − nRT1P1)

Comparing Isothermal vs Adiabatic Curves :

VP P₁, V₁, T₁ iso (T₂ = T₁) adia (T₃ < T₁)
  • For a given expansion, the Isothermal curve lies above the Adiabatic curve.
  • Area under the curve gives magnitude of work: |Wiso| > |Wadia|.
  • For adiabatic expansion curves of two different gases, the gas with the higher γ (e.g., Monoatomic > Diatomic) has a steeper curve.

22. Slopes in P-V Graphs

  • Isothermal slope : PV = K ⇒ P + V(dP/dV) = 0 ⇒ dP/dV = −P/V
  • Adiabatic slope : PVγ = K ⇒ PγVγ−1 dV + Vγ dP = 0 ⇒ dP/dV = −γ(P/V)
Slope of adiabatic P-V curve = γ × (Slope of isothermal P-V curve)
  • Comparison of Gases (Adiabatic process) : Steeper curve (higher slope) means higher γ value.
    For γ : Monoatomic (1.67) > Diatomic (1.40) > Polyatomic (1.33).
  • Expansion : Steeper slope ⇒ lower final pressure at the same volume. Curve for He (mono) will be lowest, O₂ (di) middle, NH₃ (poly) highest.
  • Compression : Steeper slope ⇒ higher final pressure at the same volume. Curve for He (mono) will be highest, O₂ (di) middle, NH₃ (poly) lowest.
Adiabatic Expansion VP NH₃ (poly) O₂ (di) He (mono) Adiabatic Compression VP He (mono) O₂ (di) NH₃ (poly)

23. Thermochemistry & Enthalpy of Reaction

  • Heat of Reaction (ΔHR) : Amount of heat evolved or absorbed when reacting species react completely as represented by a balanced chemical equation.
  • ΔHR = Σ Hf (Products) − Σ Hf (Reactants)
  • The specific name of the enthalpy depends on the process (e.g., Heat of Formation, Combustion, Neutralisation, Solution, Isomerisation).

Endothermic Reactions :

  • Heat is absorbed (+). ΔH = HP − HR = (+)ve.
  • Examples: Dissociation, Fusion, Vapourisation, Sublimation, Photochemical reactions.
Progress of RxnPE ΔH (+) HRHP

Exothermic Reactions :

  • Heat is evolved (−). ΔH = HP − HR = (−)ve.
  • Examples: Combustion, Neutralisation, Bond Formation, Solution process, Dilution process, Respiration.
Progress of RxnPE ΔH (−) HRHP

24. Standard Enthalpy of Formation (ΔH°f)

  • Change in enthalpy when one mole of a substance is formed from its constituent elements in their most stable/reference state at 1 bar pressure and (usually) 298 K.
  • The standard enthalpy of formation of elements in their reference (pure) state is assumed to be zero.
ΔH°f (reference state) = 0
  • Reference states (ΔH°f = 0) : H2(g), O2(g), Cl2(g), N2(g), C(s, graphite), S8(rhombic), P4(white), Br2(l), I2(s), Na(s), Fe(s), Zn(s), Sn(white), H⁺(aq).
  • Non-reference states (ΔH°f ≠ 0) : H(g), O(g), Br2(g), OH⁻(aq), C(s, diamond), Zn(l).

Identifying True Formation Reactions :

  • The reaction enthalpy ΔHR is equal to ΔHf ONLY if exactly 1 mole of product forms from reference-state elements.
  • Examples where ΔHR = ΔH°f :
    • C(graphite) + O2(g) → CO2(g)
    • 12 H2(g) + 12 Cl2(g) → HCl(g)
    • 12 H2(g) + 12 Br2(l) → HBr(g)
    • 18 S8(s) + O2(g) → SO2(g)
    • 32 O2(g) → O3(g)
  • Examples where ΔHR ≠ ΔH°f :
    • C(diamond) + O2(g) → CO2(g) (Diamond is not the reference state of Carbon)
    • 2 H2(g) + O2(g) → 2 H2O(l) (Forms 2 moles instead of 1 mole)
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Standard State & Reference State & Bomb Calorimeter

25. Standard State & Reference State

  • Standard state : 1 bar and 298 K.
  • Reference state : the most stable form of an element at 1 bar and the specified temperature.
ElementReference state
HydrogenH2(g)
OxygenO2(g)
ChlorineCl2(g)
BromineBr2(l)
IodineI2(s)
CarbonC (graphite)
SulphurS8 (rhombic)
PhosphorusP4 (white)
NitrogenN2(g)
SodiumNa(s)
TinSn (white)
IronFe(s)

Standard Enthalpy of Formation (ΔfH°) :

  • Enthalpy change when one mole of a substance is formed from its constituent elements in their reference states.
ΔfH° = 0 for elements in their reference state:
H2(g), O2(g), Zn(s), Br2(l), H+(aq), C(s, graphite), S8(rhombic), P4(white), Sn(white)
  • ΔfH° ≠ 0 for : H(g), O(g), Zn(l), Br2(g), OH−(aq), C(s, diamond) — these are not reference states.

26. Enthalpy of Formation — Key Relation

ΔRH° = Σ (ΔfH°)products − Σ (ΔfH°)reactants
  • ΔRH° equals ΔfH° of the product only when reactants are elements in their standard states.
Na(s) + ½ Cl2(g) → NaCl(s)  ⇒  ΔRH = (ΔfH°)NaCl
Na+(g) + Cl−(g) → NaCl(s)  ⇒  ΔRH ≠ (ΔfH°)NaCl

27. Enthalpy (Heat) of Combustion

  • The decrease in enthalpy when one mole of a substance is completely oxidised.
  • Organic compounds (containing C, H, O) burn to CO2(g) and H2O(l).
  • The final oxidation state of the central atom must be maximum (C → +4, S → +6, N → +5, P → +5).
CH4(g) + 2O2(g) → CO2(g) + 2H2O(l) ; ΔH° = −890.36 kJ/mol

Combustion of C(s) :

  • C(s) + ½ O2(g) → +2CO(g) ; ΔRH ≠ (ΔcH) of C(s)  — carbon not in max. oxidation state.
  • C(s) + O2(g) → +4CO2(g) ; ΔRH = (ΔcH) of C(s)
(ΔcH)C(s) = (ΔfH°)CO₂(g)

Combustion of H2(g) :

  • H2(g) + ½ O2(g) → H2O(l) ; ΔRH = (ΔcH) of H2(g)
(ΔcH)H₂(g) = (ΔfH°)H₂O(l)

Key relations :

ΔRH = Σ (ΔfH°)P − Σ (ΔfH°)R
ΔRH = Σ (ΔcH)R − Σ (ΔcH)P

28. Bomb Calorimeter

  • Used to measure heat of combustion at constant volume.
  • During combustion, energy is released; this energy is absorbed by the bomb and the surrounding water.
  • Components: insulated outer container filled with water, a stirrer, a thermometer, an oxygen inlet, and a central steel bomb containing the sample compound.

Key formulas :

Q = C ΔT = mbomb sbomb ΔT + mwater swater ΔT

C = heat capacity of the calorimeter (bomb + water).

ΔU = − Qn   (n = moles of substance burnt)
ΔH = ΔU + Δng RT

Δng = (moles of gaseous products) − (moles of gaseous reactants).

29. Kirchhoff's Equation

  • Relates the change in reaction enthalpy with temperature.
ΔHT₂ = ΔHT₁ + ∫T₁T₂ ΔCp dT

ΔCp = ΣCp(products) − ΣCp(reactants). If Cp values are constant, ΔHT₂ = ΔHT₁ + ΔCp(T₂ − T₁).

30. Enthalpy (Heat) of Solution

  • Heat evolved or absorbed when one mole of solute is dissolved in excess (infinite) solvent so that further dilution causes no heat change.
solute + ∞ H2O → solution ; ΔRH = ΔHsol
  • H2SO4(l) + aq → H2SO4(aq) ; ΔH = −20.2 kcal
  • KCl(s) + aq → KCl(aq) ; ΔH = +4.4 kcal
  • Heat of an ideal solution is taken as zero.

31. Enthalpy (Heat) of Dilution

  • Heat evolved or absorbed when a solution containing one mole of solute is diluted from one concentration to another.
ΔHdilution (from conc. 1 → conc. 2) = ΔH2 − ΔH1
  • HCl(g) + 10H2O → HCl·10H2O ; ΔH1 = −69.01 kJ/mol
  • HCl(g) + 25H2O → HCl·25H2O ; ΔH2 = −72.03 kJ/mol
  • HCl(g) + 40H2O → HCl·40H2O ; ΔH3 = −72.79 kJ/mol
  • HCl(g) + ∞H2O → HCl·∞H2O ; ΔH∞ = −74.85 kJ/mol
  • e.g. Dilution 10 → 40 mol H2O : ΔH = −72.79 − (−69.01) = −3.78 kJ/mol

Relation between ΔHsol, lattice enthalpy & hydration enthalpy :

ΔHsol = ΔHlattice + ΔHhydration
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Enthalpy (Heat) of Neutralisation

32. Enthalpy (Heat) of Neutralisation

  • Heat evolved when one gram equivalent of acid is completely neutralised by one gram equivalent of base in dilute solution, i.e., when one mole of H2O is formed from H+(aq) and OH−(aq).
  • ΔH°neutralisation is always negative.
H+(aq) + OH−(aq) → H2O(l) ; ΔH = −13.7 kcal = −57.3 kJ
  • This value (−57.3 kJ) holds for strong acid + strong base (complete ionisation, no extra energy cost).

Effect of weak acid / weak base :

  • Part of the heat is consumed in ionising the weak electrolyte, so |ΔHneut| < 57.3 kJ.
CombinationΔH°neutralisation
Strong acid + Strong base−13.7 kcal (−57.3 kJ)
Weak acid + Strong base−13.7 kcal + ΔH°diss(WA)
Strong acid + Weak base−13.7 kcal + ΔH°diss(WB)
Weak acid + Weak base−13.7 kcal + ΔH°diss(WA) + ΔH°diss(WB)

ΔH°diss (dissociation/ionisation enthalpy) is positive for a weak electrolyte, making the net neutralisation heat less exothermic.

33. Enthalpy of Phase Transition

Enthalpy of Fusion :

  • Enthalpy change when 1 mole of a substance converts from solid to liquid at its melting point.
ΔHfusion = Latent heat of fusion (per gram) × Molar mass

e.g. H2O(s) → H2O(l) ; ΔH = 1.44 kcal mol−1

Enthalpy of Vaporisation :

  • Enthalpy change when 1 mole of a substance converts from liquid to gas at its boiling point.
ΔHvap = Latent heat of vaporisation (per gram) × Molar mass

e.g. H2O(l) → H2O(g) ; ΔH = 10.5 kcal mol−1

Enthalpy of Sublimation :

  • Enthalpy change when 1 mole of a solid converts directly into vapour at a temperature below its melting point.

e.g. I2(s) → I2(g) ; ΔH = 14.9 kcal mol−1

34. Enthalpy of Atomisation

  • Enthalpy change when 1 mole of a compound (solid, liquid or gas) is dissociated into its constituent atoms in the gaseous state.
  • Restriction : (i) 1 mole of the compound, (ii) products must be gaseous atoms.

Examples :

  • H2(g) → 2 H(g) ; ΔHR = ΔHatom(H2(g))
  • O3(g) → 3 O(g) ; ΔHR = ΔHatom(O3(g))
  • CH4(g) → C(g) + 4 H(g) ; ΔHR = ΔHatom(CH4(g))
  • Br2(l) → 2 Br(g) ; ΔHR = ΔHatom(Br2(l))
  • I2(s) → 2 I(g) ; ΔHR = ΔHatom(I2(s))

35. Bond Dissociation Energy (BDE)

  • Energy required to break 1 mole of a particular bond between atoms in the gaseous state, separating the atoms into gaseous state, at 1 atm and specified temperature.

e.g. H–H(g) → 2 H(g) ; ΔH = 433 kJ mol−1
H–I(g) → H(g) + I(g) ; ΔH = 299 kJ mol−1

Atomisation vs BDE :

  • In BDE: both reactants and products are in gaseous state.
  • In atomisation: products are gaseous, but reactant may or may not be gaseous.
ΔHatom(Br2(l)) > BDE(Br–Br)
(because atomisation from liquid includes energy to vaporise first)

Br2(l) → 2 Br(g) ; ΔHatom  vs  Br–Br(g) → 2 Br(g) ; EBr–Br  ⇒  ΔHatom > EBr–Br

  • Similarly for I2: ΔHatom(I2(s)) > BDE(I–I)

Single bond vs multiple bonds of same type :

  • If a molecule has only one bond of a particular type, BDE is an absolute value.
  • If a molecule has more than one bond of the same type, BDE is an average value.

e.g. In H2: H–H(g) → 2 H(g) — single bond, absolute value.

In H2O: first O–H bond breaks with energy a, second with energy b.
εO–H = a + b2

In CH4: four C–H bonds break with energies a, b, c, d.
εC–H = a + b + c + d4

36. Using Bond Energies to Find ΔHR

ΔHR = ∑ (Bond energies of bonds broken) − ∑ (Bond energies of bonds formed)

37. Hess's Law of Constant Heat Summation

  • A consequence of the first law of thermodynamics.
  • "The enthalpy change in a chemical or physical process is the same whether the process is carried out in one step or in several steps."
  • This is because enthalpy change is independent of the path followed.

Example :

C(graphite) + O2(g) → CO2(g) ; ΔH

  • Step 1 : C(graphite) + 12 O2(g) → CO(g) ; ΔH1
  • Step 2 : CO(g) + 12 O2(g) → CO2(g) ; ΔH2
ΔH = ΔH1 + ΔH2

38. Resonance Energy (RE)

  • The theoretical ΔHf is calculated assuming a Kekulé-type structure (no delocalisation).
  • The experimental ΔHf differs because of resonance stabilisation.
RE = (ΔHf)experimental − (ΔHf)theoretical
RE = (ΔHhydrogenation)expected − (ΔHhydrogenation)actual
  • RE is always negative (the actual molecule is more stable than the hypothetical structure).
Page 8
Born–Haber Cycle & Qualitative Comparison of Entropy

39. Born–Haber Cycle

  • Used to calculate lattice enthalpy (LE) of an ionic solid indirectly, since it cannot be measured directly.

For NaCl :

  • Na(s) + 12 Cl2(g) → NaCl(s)   [ΔHf]
  • Steps: Na(s) →ΔHsub Na(g) →IE Na+(g)
  • 12 Cl2(g) →12 BE Cl(g) →ΔHeg Cl−(g)
  • Na+(g) + Cl−(g) →LE NaCl(s)
ΔHf = ΔHsub + IE + 12 BE + ΔHeg + LE

For Al2O3 :

  • 2 Al(s) + 32 O2(g) → Al2O3(s)
  • Steps involve: 2 ΔHsub(Al), then 2 I1 + 2 I2 + 2 I3 for aluminium; 32 O2 → 3 O(g), then 3 ΔHeg1 and 3 ΔHeg2 for oxygen; finally lattice enthalpy LE to form the solid.

40. Limitations of the First Law

  • The First Law cannot explain why some processes occur on their own and others do not.
  • It cannot explain the direction of heat flow — it can only calculate q, W, ΔU, etc.
  • It cannot predict the spontaneity of a process.

41. Proposed Criteria for Spontaneity

1. Enthalpy change (ΔHsys) :

  • "Processes which are exothermic (ΔHsys < 0) are always spontaneous" — this is NOT always true (counter-examples exist).

2. Entropy change of system (ΔSsys) :

  • Entropy (S) is a measure of randomness / disorder.
  • Liquid (less random, S1) → Gas (more random, S2) : S2 − S1 > 0 ⇒ ΔSsys > 0.

3. Entropy change of Universe (ΔSuniv) :

ΔSuniv = ΔSsystem + ΔSsurrounding > 0   (for a spontaneous process)

42. Second Law of Thermodynamics

  • For any irreversible (spontaneous) process, the entropy of the universe is increasing.
  • Transfer of heat from a cold body to a hot body cannot occur without an external agent performing work.
  • Any process occurring on its own is thermodynamically irreversible.

43. Entropy — Definition & Properties

  • Entropy (S) = degree of randomness or disorderliness of a system.
  • Change in entropy is the capacity for spontaneous changes in a system.
  • Entropy is a state function.
  • Entropy is an extensive property.
  • ΔS is also a state function.
ΔSrev = ΔSirr

(Between the same two states, ΔS is the same whether the path is reversible or irreversible, because S is a state function.)

44. Qualitative Comparison of Entropy

i) Phase :

Ssolid < Sliquid < Sgas
  • Solid → Liquid : ΔS > 0
  • Liquid → Gas : ΔS > 0
  • Gas → Liquid : ΔS < 0
  • Liquid → Solid : ΔS < 0
  • Solid → Gas (sublimation) : ΔS > 0

ii) Volume constant, Temperature increased :

  • Temperature ↑ ⇒ Entropy ↑ ⇒ ΔS > 0

iii) Temperature constant, Volume increased :

  • Volume ↑ ⇒ Entropy ↑ ⇒ ΔS > 0

iv) For a chemical reaction (gaseous moles rule) :

  • aA(g) + bB(g) → cC(g) + dD(g)
Δng = (c + d) − (a + b)
  • Δng > 0 ⇒ ΔS > 0
  • Δng < 0 ⇒ ΔS < 0
  • Note : Even when Δng = 0, heteronuclear diatomic molecules have more entropy than homonuclear ones.
    e.g. H2(g) + Cl2(g) → 2 HCl(g) ; Δng = 0, yet ΔS > 0.

v) Different gases — Atomicity rule :

  • More atomicity ⇒ more entropy.
  • SO2 (atomicity 3) > O2 (atomicity 2)
  • CH4 (atomicity 5) > O3 (atomicity 3)

vi) Same atomicity — Molecular weight rule :

  • Higher molecular weight ⇒ higher entropy.
  • SO2 > CO2 (both atomicity 3, but M.Wt of SO2 > CO2)

vii) Isomers of hydrocarbons :

  • Branched isomers have less entropy than their straight-chain isomers.
  • e.g. For C5H12 isomers : S(n-pentane) > S(isopentane) > S(neopentane)

viii) Mixing / Dissolution :

  • During mixing of solute in solvent, entropy increases : ΔSsolution > 0.

45. Quantitative Estimation of Entropy

Entropy change of system :

dSsys = dqrevT

dqrev = heat exchanged by the system (reversible path) ; T = temperature at which heat is exchanged.

ΔSsys = ∫T₁T₂ dqrevT

Entropy change of surroundings :

ΔSsurr = − ΔHsysTsurr

46. Third Law of Thermodynamics

  • As the temperature of a system approaches absolute zero, the entropy of a perfect crystal approaches zero.
S → 0   as   T → 0 K
  • According to the 3rd Law, it is impossible to reach 0 K.
  • It provides a reference point for absolute entropy.
  • It helps in the calculation of absolute entropy of a substance.
  • Fails for imperfect crystals and amorphous solids.
Page 9
Entropy Change on Heating / Cooling a Substance

47. Entropy Change on Heating / Cooling a Substance

ΔS = m s ln T2T1   (using specific heat, s)   or   ΔS = n C ln T2T1   (using molar heat capacity, C)

m = mass, s = specific heat (J g⁻¹ K⁻¹), n = moles, C = Cp or Cv as appropriate.

  • For a reversible process where Tsurr always equals Tsys: ΔSsurr = −ΔSsys, so ΔStotal = 0.
  • For an irreversible heating using a reservoir at fixed Tres:
    ΔSsurr = −qsysTres = −m s (T2 − T1)Tres   and   ΔStotal > 0.

48. Entropy Change — Phase Transformations

Melting (Fusion) :

  • Solid → Liquid at the melting point Ttrans
ΔSsys = ΔHfusTtrans   (per mol)

Boiling (Vaporisation) :

  • Liquid → Vapour at the boiling point Ttrans
ΔSsys = ΔHvapTtrans   (per mol)

Sublimation :

  • Solid → Vapour at the sublimation temperature Ttrans
ΔSsys = ΔHsubTtrans   (per mol)

49. Reversible Phase Change — ΔSuniv = 0

  • When a phase change occurs at the transition temperature with surroundings at the same temperature, the process is reversible.
ΔSsys = nΔHtransT  ;  ΔSsurr = − nΔHtransT  ;  ΔSuniv = 0

50. Entropy of the Universe — Criterion of Spontaneity

ΔSuniv = ΔSsys + ΔSsurr
  • ΔSsurr = −qsysTsurr   (surroundings are large, so Tsurr = const; the process in the surroundings is always reversible).
  • At constant P: qsys = ΔHsys, so ΔSsurr = −ΔHsysTsurr
ConditionNature
ΔSuniv > 0Spontaneous
ΔSuniv = 0Reversible (equilibrium)
ΔSuniv < 0Non-spontaneous
  • ΔSsys or ΔSsurr alone is not responsible for spontaneity — only ΔSuniv decides.

51. Entropy Change for an Ideal Gas (General Formula)

ΔSsys = n Cv ln T2T1 + n R ln V2V1

This is a state function — valid for any process connecting (T₁, V₁) and (T₂, V₂).

a) Isothermal Process (T₂ = T₁) :

ΔSsys = n R ln V2V1
  • For a reversible isothermal expansion: ΔSsurr = −n R ln(V2/V1), so ΔStotal = 0.
  • For free expansion into vacuum: q = 0, so ΔSsurr = 0 and ΔSuniv = ΔSsys.

b) Reversible Adiabatic Process :

  • qrev = 0, so ΔSsys = 0 (isentropic). Both temperature and volume change, but the two terms in the general formula cancel.

c) Isochoric Process (V₂ = V₁) :

ΔSsys = n Cv ln T2T1
  • ΔSsurr = −n Cv (T2 − T1)Tsurr

d) Isobaric Process (P = const, V ∝ T) :

  • At constant P: V2/V1 = T2/T1.
ΔSsys = n Cv ln T2T1 + n R ln T2T1 = n (Cv + R) ln T2T1 = n Cp ln T2T1
  • ΔSsurr = −n Cp (T2 − T1)Tsurr

52. Isothermal Process (T1 = T2)

  • For an ideal gas: ΔU = 0 ⇒ q = −w
  • Temperature factor vanishes (ln 1 = 0).
ΔSsys = nR ln V2V1 = nR ln P1P2

Reversible :

  • qsys = −W = nRT ln(V2/V1) ⇒ ΔSsurr = − qsysT = − nRT ln(V2/V1)T = −nR ln V2V1
ΔSuniv = 0   (reversible)

Irreversible :

  • ΔSsys = nR ln V2V1   (same states ⇒ same ΔSsys, since entropy is a state function)
  • ΔSsurr = − Pext(V2 − V1)T
ΔSuniv = nR ln V2V1 − Pext(V2 − V1)T   > 0
Page 10
Adiabatic Process — Reversible & Relation between ΔG° and Keq

53. Adiabatic Process — Reversible

  • q = 0 ⇒ dqrev = 0
ΔSsys = 0
  • Proof: ΔSsys = nR ln V2V1 + nCv ln T2T1
  • Using TVγ−1 = const ⇒ T2T1 = (V1V2)γ−1
  • = nR ln V2V1 + n(γ−1)Cv ln V1V2
  • Since (γ−1)Cv = RCv · Cv = R ⇒ nR ln V2V1 + nR ln V1V2 = 0
  • q = 0 (no heat reaches the surroundings) ⇒ ΔSsurr = 0
ΔSuniv = 0   (reversible adiabatic)

54. Adiabatic Process — Irreversible

  • ΔSsurr = 0 (no heat exchange with surroundings).
  • ΔSsys ≠ 0 for an irreversible adiabatic process (final state differs from reversible case).
ΔSsys = nCv ln T2T1 + nR ln V2V1
  • Entropy is a state function: (ΔSsys)rev from state 1→2 = (ΔSsys)irrev from state 1→2 (same endpoints).
  • But in irreversible adiabatic, the final state (state 3) is different from the reversible final state (state 2), so ΔSirr ≠ ΔSrev.

Work in adiabatic processes :

  • Since q = 0: ΔU = W. As ΔU is a state function, if initial and final states are the same, Wrev = Wirrev.
  • However, in general the irreversible adiabatic reaches a different final state, so W is not a state function.

55. Gibbs Energy (G)

  • Gibbs energy is defined at constant temperature and pressure to predict spontaneity in terms of the system alone.
  • It measures the capacity of a system to do useful (non-PV) work; it is that part of total energy which can be converted into useful work.

Derivation from ΔSuniv :

  • ΔSuniv = ΔSsys + ΔSsurr = ΔSsys − ΔHsysT
  • Multiply by −T:   −TΔSuniv = ΔHsys − TΔSsys
ΔGsys = ΔHsys − TΔSsys
ConditionNature
ΔG < 0Spontaneous (forward)
ΔG = 0Equilibrium
ΔG > 0Non-spontaneous

56. Effect of Temperature on Spontaneity (Four Cases)

CaseΔHΔSΔG = ΔH − TΔSSpontaneity
1< 0> 0Always < 0Spontaneous at all T
2> 0< 0Always > 0Never spontaneous
3< 0< 0< 0 at low T, > 0 at high TSpontaneous at lower T
4> 0> 0> 0 at low T, < 0 at high TSpontaneous at higher T
  • Case 3: At ΔG = 0, T = ΔHΔS = maximum temperature till which the process is spontaneous.
  • Case 4: At ΔG = 0, T = ΔHΔS = minimum temperature above which the process is spontaneous.

57. Relation between ΔG° and Keq

ΔG = ΔG° + RT ln Q
  • At equilibrium: Q = Keq and ΔG = 0.
ΔG° = −RT ln Keq

58. Thermodynamic Partial Derivatives (Standard Results)

Partial DerivativeEquals
(∂G/∂T)P−S
(∂H/∂T)PCp
(∂U/∂T)VCv

59. Quick Formula Revision

QuantityFormula
First lawΔU = q + W
EnthalpyH = U + PV ; ΔH = ΔU + ΔngRT
Work (constant Pext)W = −Pext(V2 − V1)
Reversible isothermal workW = −2.303 nRT log(V2/V1) = −2.303 nRT log(P1/P2)
Reversible adiabaticPVγ, TVγ−1, TP(1−γ)/γ = constant
Adiabatic workW = nCv(T2 − T1) = (P2V2 − P1V1)/(γ − 1)
Heat capacitiesCp − Cv = R ; γ = Cp/Cv
Gas mixtureCv,mix = ΣniCv,i/Σni ; Σn/(γmix − 1) = Σ ni/(γi − 1)
Heat of reactionΔHR = ΣΔHf(P) − ΣΔHf(R) = ΣΔHc(R) − ΣΔHc(P)
From bond energiesΔHR = Σ BE(broken) − Σ BE(formed)
Neutralisation (SA + SB)−57.3 kJ (−13.7 kcal) per mol H2O
EntropyΔS = qrev/T ; ΔStrans = ΔHtrans/Ttrans
Ideal gas entropyΔS = nCv ln(T2/T1) + nR ln(V2/V1)
SurroundingsΔSsurr = −qsys/Tsurr
Gibbs energyΔG = ΔH − TΔS ; ΔG° = −RT ln K ; ΔG = ΔG° + RT ln Q

Key Points :

  • State functions (U, H, S, G, P, V, T) depend only on the state; q and W depend on the path.
  • Sign convention : heat absorbed and work done on the system are positive.
  • |Wrev| > |Wirr| in expansion ; |Wirr| > |Wrev| in compression.
  • Free expansion of an ideal gas : W = 0, q = 0, ΔU = 0.
  • ΔHf° = 0 for elements in their reference state (graphite, not diamond).
  • Spontaneous : ΔSuniv > 0, or ΔG < 0 at constant T and P.