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Chapter 11 · Thermodynamics — NCERT Class 11 Physics
The Zeroth Law states: "Two systems in thermal equilibrium with a third system separately are in thermal equilibrium with each other." This establishes the concept of temperature as the common thermodynamic variable. Formulated by R.H. Fowler in 1931.
ΔQ = heat supplied to system, ΔU = change in internal energy, ΔW = work done by system. It is the general law of conservation of energy applied to thermodynamic systems. Note: ΔU is a state variable; ΔQ and ΔW are path-dependent.
For an ideal gas (negligible intermolecular forces), internal energy U = sum of kinetic energies of molecules, which depends only on temperature T. This is why ΔU = 0 in isothermal processes for ideal gases. For real gases, U depends on T and V.
Isothermal = T = constant → ΔU = 0 (for ideal gas). From First Law: ΔQ = ΔU + ΔW = 0 + ΔW → ΔQ = ΔW. All heat supplied is converted to work. PV = constant (Boyle's Law), W = μRT ln(V₂/V₁).
Adiabatic: thermally insulated system. Work done by gas decreases internal energy → temperature falls (expansion) or rises (compression). PVᵞ = constant, where γ = Cp/Cv.
PV = constant is Boyle's Law (isothermal). The adiabatic exponent γ > 1 always, so the adiabatic curve is steeper than the isothermal curve on a P-V diagram. For monatomic gas γ = 5/3; diatomic γ = 7/5.
Isochoric = V = constant → no work done (ΔW = PΔV = 0). From First Law: ΔQ = ΔU. All heat absorbed goes entirely to increase internal energy. Heat supplied = m·Cv·ΔT.
At constant pressure, extra heat is needed to do work against expansion (PΔV = μRΔT for 1 mole). So Cp > Cv always. R = 8.31 J mol⁻¹K⁻¹. This is known as Mayer's relation. γ = Cp/Cv > 1.
In a cyclic process the system returns to its initial state. Since U is a state variable (path-independent), ΔU = U_final − U_initial = 0. Therefore from First Law: ΔQ = ΔW — the total heat absorbed equals the total work done by the system.
Internal energy U is a state variable — its value depends only on the current state, not on the path taken. Heat Q and Work W are path-dependent quantities (not state variables). P, V, T, and m are also state variables.
Kelvin-Planck: "No process is possible whose sole result is the absorption of heat from a reservoir and its complete conversion to work." → No perfect heat engine (η = 100%) exists. Clausius: Heat cannot spontaneously flow from cold to hot (option A is Clausius statement).
T₁ = source (hot), T₂ = sink (cold). Since T₂ < T₁, η < 1 always. For η = 1 (100%), T₂ = 0 K (absolute zero) — physically impossible. Carnot efficiency is the maximum possible for any engine between two temperatures.
All four steps must be reversible (quasi-static, no friction) making the Carnot engine the most efficient possible engine.
A reversible process requires: (1) Quasi-static — infinitely slow, system in equilibrium at every stage; (2) No dissipative effects — no friction, viscosity, etc. In practice, all real processes are irreversible to some degree.
Free expansion of gas into vacuum is irreversible — it is a rapid, non-quasi-static process where the gas passes through non-equilibrium states. It cannot be reversed spontaneously. Other irreversible examples: diffusion, combustion, heat flow across finite temperature differences.
Since PV = μRT → P = μRT/V. W = ∫P dV = μRT∫dV/V = μRT ln(V₂/V₁). For expansion V₂ > V₁ → W > 0 (gas does work). Option (C) is for adiabatic process. Option (D) is for isobaric.
An adiabatic wall is a perfect insulator — it does not allow heat (energy) flow. A diathermic wall is the opposite — it allows heat to flow until thermal equilibrium is reached. The Zeroth Law uses diathermic walls conceptually.
In adiabatic compression: ΔQ = 0. Work is done on the gas (ΔW < 0) → ΔU = −ΔW > 0 → internal energy increases → temperature increases. This is why a bicycle pump heats up when inflating a tyre rapidly.
Monatomic gases have only 3 translational degrees of freedom. Diatomic gases have 2 additional rotational degrees of freedom (5 total). More degrees of freedom → higher Cv → lower γ.
Adiabatic curve is steeper than isothermal. Isothermal: PV = const → slope = −P/V. Adiabatic: PVᵞ = const → slope = −γP/V. Since γ > 1, the adiabatic slope is steeper. This is because during adiabatic expansion, temperature also falls, reducing pressure more.
Free expansion into vacuum: ΔQ = 0 (insulated), ΔW = 0 (no external pressure to work against). By First Law: ΔU = ΔQ − ΔW = 0. For ideal gas, U depends only on T → temperature remains unchanged. (This is NOT a reversible process.)
Carnot's theorem: No engine working between two given temperatures can have efficiency greater than that of the Carnot engine. The Carnot efficiency η = 1 − T₂/T₁ is the maximum possible efficiency for any heat engine operating between T₁ and T₂. All real engines are less efficient due to irreversibility.
Q and W are path-dependent — different paths from the same initial to final state give different Q and W values. Only their difference (ΔQ − ΔW = ΔU) is path-independent. Saying "a gas has a certain amount of heat" is meaningless — heat is energy in transit.
This is a universal relation independent of the nature of the working substance. It is used to define a truly universal thermodynamic temperature scale. Efficiency η = 1 − Q₂/Q₁ = 1 − T₂/T₁.
Using Mayer's relation Cp = Cv + R. For monatomic gas (3 translational DOF): Cv = (3/2)R → Cp = 5R/2 ≈ 20.8 J mol⁻¹K⁻¹. This matches experimental value for He (20.8).
The geyser burns approximately 15.75 g of fuel per minute to heat the water.
Insulated walls + piston with sand = adiabatic process. γ for H₂ = 1.4.
Always convert temperatures to Kelvin before using the Carnot efficiency formula.
Most of the heat (93%) goes to increase internal energy (breaking intermolecular bonds). Only 7% does work against atmospheric pressure.
To increase efficiency from 40% to 60%, the source temperature must be raised from 500 K to 750 K (an increase of 250 K).
High COP (≈10) means very efficient refrigerator — just ~99 J of work removes 1000 J of heat from cold space.
In isothermal compression, all work done on the gas is released as heat to surroundings. Temperature remains constant.
This is a remarkable result — only a Carnot (reversible) engine can achieve the theoretical maximum efficiency. All real engines have lower efficiency due to irreversible losses.