Thermodynamics

Master laws of thermodynamics, thermodynamic processes, heat engines, and entropy for JEE Physics.

Thermodynamics deals with heat, work, and the relationship between them. It’s fundamental to understanding engines, refrigerators, and natural processes.

Overview

graph TD
    A[Thermodynamics] --> B[Zeroth Law]
    A --> C[First Law]
    A --> D[Second Law]
    B --> B1[Thermal Equilibrium]
    C --> C1[Energy Conservation]
    C --> C2[Processes]
    D --> D1[Heat Engines]
    D --> D2[Entropy]

Basic Concepts

System and Surroundings

  • System: Part of universe under study
  • Surroundings: Everything outside the system
  • Boundary: Separates system from surroundings

Types of Systems

TypeEnergy ExchangeMatter Exchange
OpenYesYes
ClosedYesNo
IsolatedNoNo

State Variables

  • Intensive: Independent of amount (T, P, density)
  • Extensive: Depends on amount (V, U, S, m)

Zeroth Law

If system A is in thermal equilibrium with system C, and system B is in thermal equilibrium with system C, then A and B are in thermal equilibrium with each other.

This law defines temperature as a measurable quantity.

First Law of Thermodynamics

$$\boxed{Q = \Delta U + W}$$

or equivalently:

$$\boxed{dU = dQ - dW}$$

where:

  • $Q$ = Heat added to system
  • $\Delta U$ = Change in internal energy
  • $W$ = Work done by system

Sign Convention

QuantityPositiveNegative
QHeat absorbedHeat released
WWork done by systemWork done on system
ΔUInternal energy increasesInternal energy decreases

Internal Energy

For an ideal gas:

$$U = \frac{f}{2}nRT$$

where $f$ = degrees of freedom

Gas Typef$C_V$$C_P$$\gamma$
Monatomic3$\frac{3}{2}R$$\frac{5}{2}R$1.67
Diatomic5$\frac{5}{2}R$$\frac{7}{2}R$1.4
Polyatomic6+$\frac{6}{2}R+$$\frac{8}{2}R+$1.33

Mayer’s Relation

$$\boxed{C_P - C_V = R}$$ $$\gamma = \frac{C_P}{C_V} = 1 + \frac{2}{f}$$

Thermodynamic Processes

Isobaric Process (Constant Pressure)

$$W = P\Delta V = nR\Delta T$$ $$Q = nC_P\Delta T$$ $$\Delta U = nC_V\Delta T$$

Isochoric Process (Constant Volume)

$$W = 0$$ $$Q = \Delta U = nC_V\Delta T$$

Isothermal Process (Constant Temperature)

$$\Delta U = 0$$ $$Q = W = nRT\ln\frac{V_2}{V_1} = nRT\ln\frac{P_1}{P_2}$$
JEE Tip
In isothermal process, internal energy doesn’t change because temperature is constant. All heat added is converted to work.

Adiabatic Process (No Heat Exchange)

$$Q = 0$$ $$\Delta U = -W$$

Equations:

$$PV^\gamma = \text{constant}$$ $$TV^{\gamma-1} = \text{constant}$$ $$P^{1-\gamma}T^\gamma = \text{constant}$$

Work done:

$$W = \frac{P_1V_1 - P_2V_2}{\gamma - 1} = \frac{nR(T_1 - T_2)}{\gamma - 1}$$

Process Summary

graph TD
    A[Thermodynamic Processes] --> B["Isobaric: P constant
W = PΔV"] A --> C["Isochoric: V constant
W = 0"] A --> D["Isothermal: T constant
ΔU = 0"] A --> E["Adiabatic: Q = 0
PVᵞ = constant"]
ProcessConditionWQΔU
IsobaricP = const$P\Delta V$$nC_P\Delta T$$nC_V\Delta T$
IsochoricV = const0$nC_V\Delta T$$nC_V\Delta T$
IsothermalT = const$nRT\ln\frac{V_2}{V_1}$W0
AdiabaticQ = 0$\frac{nR\Delta T}{1-\gamma}$0$-W$

Second Law of Thermodynamics

Kelvin-Planck Statement

It is impossible to construct an engine operating in a cycle that converts all heat into work.

Clausius Statement

It is impossible to transfer heat from cold body to hot body without external work.

Heat Engines

Efficiency

$$\boxed{\eta = \frac{W}{Q_H} = \frac{Q_H - Q_C}{Q_H} = 1 - \frac{Q_C}{Q_H}}$$

where:

  • $Q_H$ = Heat absorbed from hot reservoir
  • $Q_C$ = Heat rejected to cold reservoir
  • $W$ = Work done by engine

Carnot Engine

Maximum efficiency heat engine operating between two temperatures.

$$\boxed{\eta_{Carnot} = 1 - \frac{T_C}{T_H}}$$

Carnot Cycle:

  1. Isothermal expansion
  2. Adiabatic expansion
  3. Isothermal compression
  4. Adiabatic compression
Common Mistake
Carnot efficiency depends only on temperatures, not on the working substance. Real engines always have lower efficiency.

Refrigerator

A heat engine running in reverse.

Coefficient of Performance (COP)

$$\boxed{COP = \frac{Q_C}{W} = \frac{Q_C}{Q_H - Q_C}}$$

For Carnot refrigerator:

$$COP_{Carnot} = \frac{T_C}{T_H - T_C}$$

Entropy

Definition

$$dS = \frac{dQ_{rev}}{T}$$

Change in Entropy

$$\Delta S = \int \frac{dQ_{rev}}{T}$$

For isothermal process:

$$\Delta S = nR\ln\frac{V_2}{V_1}$$

Second Law in Terms of Entropy

For isolated system:

$$\Delta S_{universe} \geq 0$$
  • Reversible process: $\Delta S = 0$
  • Irreversible process: $\Delta S > 0$

Practice Problems

  1. One mole of ideal gas at 300 K expands isothermally to double its volume. Find work done and heat absorbed.

  2. An engine operating between 500 K and 300 K has efficiency 30%. Is it a reversible engine?

  3. A gas is compressed adiabatically to half its volume. If initial temperature is 27°C, find final temperature. (γ = 1.4)

  4. Calculate entropy change when 1 kg of ice at 0°C melts. (L = 334 kJ/kg)

Quick Check
Why is it impossible to reach absolute zero temperature?

Further Reading