Thermodynamics

Learning Objectives

  • Differentiate between temperature, heat, and internal energy.
  • Calculate thermal expansion and heat required for temperature changes and phase changes.
  • Explain the three mechanisms of heat transfer: conduction, convection, and radiation.
  • Understand and apply the laws of thermodynamics (Zeroth, First, Second, and Third).
  • Analyze thermodynamic processes and calculate the efficiency of heat engines.
  • Relate macroscopic gas properties to microscopic behavior using the Ideal Gas Law and Kinetic Theory.
Thermodynamics is the branch of physics that deals with heat, work, and temperature, and their relation to energy, radiation, and physical properties of matter. It is fundamental in designing engines, HVAC systems, and power plants.

Temperature and Heat

Temperature and Heat Concepts

In everyday language, "heat" and "temperature" are often used interchangeably. In physics, they have very precise and distinct meanings.

Temperature (TT)

A macroscopic measure of the average random microscopic kinetic energy of the particles in a substance. It determines the direction of spontaneous heat transfer. The SI unit is the Kelvin (K), but Celsius (^\circC) is also widely used in engineering.

TK=TC+273.15 T_K = T_C + 273.15

Heat (QQ)

The transfer of energy between a system and its environment due solely to a temperature difference. Heat always flows spontaneously from an object at higher temperature to one at lower temperature. The SI unit is the Joule (J).

Heat vs. Internal Energy

An object does not contain "heat". It contains internal energy. Heat is only energy that is in transit.

Thermal Expansion and Heat Capacity

Thermal Expansion and Heat Capacity Concepts

Most materials expand when heated and contract when cooled. For solids and liquids, this expansion is typically proportional to the temperature change.

Linear Thermal Expansion

Calculates the change in length of a solid due to a change in temperature.

ΔL=αL0ΔT\Delta L = \alpha L_0 \Delta T

Variables

SymbolDescriptionUnit
ΔL\Delta LChange in lengthm
α\alphaCoefficient of linear expansionK1K^{-1}
L0L_0Initial lengthm
ΔT\Delta TChange in temperatureK

Volume Thermal Expansion

Calculates the change in volume of a substance due to a change in temperature.

ΔV=βV0ΔT\Delta V = \beta V_0 \Delta T

Variables

SymbolDescriptionUnit
ΔV\Delta VChange in volumem3m^3
β\betaCoefficient of volume expansionK1K^{-1}
V0V_0Initial volumem3m^3
ΔT\Delta TChange in temperatureK

Specific Heat Capacity (cc)

Specific Heat Capacity (cc) Concepts

The amount of heat (QQ) required to change the temperature of a substance depends on its mass (mm) and a material property called specific heat capacity.

Specific Heat Equation

Calculates the heat required to change the temperature of a mass.

Q=mcΔTQ = mc\Delta T

Variables

SymbolDescriptionUnit
QQHeat added or removedJ
mmMasskg
ccSpecific heat capacityJ/(kgK)J/(kg \cdot K)
ΔT\Delta TChange in temperatureK

Specific Heat Capacity

Water has a very high specific heat (4186 J/kgK4186 \text{ J/kg}\cdot\text{K}), meaning it takes a lot of energy to change its temperature.

Latent Heat (LL)

Latent Heat (LL) Concepts

When a substance undergoes a phase change (like melting or boiling), heat is added or removed without any change in temperature. The energy goes into breaking or forming intermolecular bonds.

Latent Heat

Calculates the heat required to change the phase of a substance without changing its temperature.

Q=mLQ = mL

Variables

SymbolDescriptionUnit
QQHeat added or removedJ
mmMass of the substancekg
LLLatent heat of fusion or vaporizationJ/kg

Mechanisms of Heat Transfer

Mechanisms of Heat Transfer Concepts

There are three fundamental mechanisms by which heat is transferred:

  • Conduction: Heat transfer through stationary matter by physical contact (e.g., a metal spoon getting hot in soup).
  • Convection: Heat transfer by the macroscopic movement of a fluid (e.g., hot air rising, water circulating in a pot). Natural convection is driven by buoyant forces, while forced convection uses pumps or fans.
  • Radiation: Heat transfer by electromagnetic waves (e.g., feeling the heat from the sun or a fire). Does not require a medium.

Fourier's Law of Heat Conduction

Calculates the rate of heat transfer through a material via conduction.

P=Qt=kAΔTLP = \frac{Q}{t} = kA \frac{\Delta T}{L}

Variables

SymbolDescriptionUnit
PPRate of heat transfer (Power)W
kkThermal conductivity of the materialW/(mK)W/(m\cdot K)
AACross-sectional aream2m^2
ΔT\Delta TTemperature difference across the materialK or CK \text{ or } ^\circ\text{C}
LLThickness of the materialm

Stefan-Boltzmann Law of Radiation

Calculates the power radiated by a black body or object.

P=σeAT4P = \sigma e A T^4

Variables

SymbolDescriptionUnit
PPRadiated powerW
σ\sigmaStefan-Boltzmann constant5.67×108 W/(m2K4)5.67 \times 10^{-8} \text{ W}/(\text{m}^2\cdot\text{K}^4)
eeEmissivity of the objectdimensionless(0 to 1)dimensionless (0 \text{ to } 1)
AASurface aream2m^2
TTAbsolute temperatureK

Civil Engineering Applications of Heat Transfer

The Laws of Thermodynamics

The Laws of Thermodynamics Concepts

These four empirical laws govern all macroscopic interactions involving energy and temperature.

The Zeroth Law: Thermal Equilibrium

The Zeroth Law: Thermal Equilibrium Concepts

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

This law defines temperature: two systems in thermal equilibrium have the same temperature.

The First Law: Conservation of Energy

The First Law: Conservation of Energy Concepts

The First Law is the principle of conservation of energy applied to thermal systems. It states that the change in a system's internal energy (ΔU\Delta U) is equal to the net heat added to the system (QQ) minus the net work done by the system on its surroundings (WW).

The First Law of Thermodynamics

Conservation of energy applied to thermal systems.

ΔU=QW\Delta U = Q - W

Variables

SymbolDescriptionUnit
ΔU\Delta UChange in internal energy of the systemJ
QQNet heat added to the systemJ
WWNet work done by the systemJ

Sign Conventions for the First Law

Sign conventions are critical here:

  • +Q+Q: Heat is added to the system.
  • Q-Q: Heat is removed from the system.
  • +W+W: Work is done by the system (it expands).
  • W-W: Work is done on the system (it is compressed).

Work Done by a Gas

Calculates the work done by a gas expanding or compressing against a pressure.

W=ViVfPdVW = \int_{V_i}^{V_f} P \, dV

Variables

SymbolDescriptionUnit
WWWork done by the gasJ
PPPressure of the gasPa
Vi,VfV_i, V_fInitial and final volumesm3m^3

Work Done on a P-V Diagram

The work done by a gas is equal to the area under the curve on a Pressure-Volume (P-V) diagram.

Thermodynamic Processes

Thermodynamic Processes Concepts

When a gas changes state (pressure, volume, temperature), it follows a specific process. The First Law applies to all of them, but simplifies uniquely for each:

  • Isothermal Process (Constant Temperature): ΔT=0\Delta T = 0, so ΔU=0\Delta U = 0 (for an ideal gas). Therefore, Q=WQ = W. Heat added is entirely converted to work done by the gas.
  • Isobaric Process (Constant Pressure): W=PΔVW = P \Delta V. Heat added changes both internal energy and does work.
  • Isochoric (Isovolumetric) Process (Constant Volume): ΔV=0\Delta V = 0, so W=0W = 0. Therefore, ΔU=Q\Delta U = Q. All heat added goes into increasing the internal energy.
  • Adiabatic Process (No Heat Transfer): Q=0Q = 0. Therefore, ΔU=W\Delta U = -W. If the gas expands and does work, its internal energy (and thus temperature) must decrease.

Interactive Simulation

Use this thermodynamic cycle model to connect heat, work, and state changes on a process path.

Interactive Physics Simulation

Thermodynamics PV Cycle & Heat Engine Simulator

Select standard thermodynamic cycle profiles (Carnot, Otto, Brayton). Adjust compression ratios, gas parameters, and temperature limits to analyze efficiency.

6.5
850 K
300 K
1.40
Cycle Thermal Efficiency Formula
ηCarnot=1TCTH\eta_{Carnot} = 1 - \frac{T_C}{T_H}

The Carnot cycle represents the absolute maximum theoretical efficiency possible for any heat engine operating between TH and TC. Larger compression/pressure ratios yield higher overall cycle thermal efficiency.

Heat input (Qin)
13,227.8 J
Net Work output (Wnet)
8,559.2 J
Engine Efficiency (η)
64.7 %
Carnot Max Limit (ηmax)
64.7 %

The Second Law: Entropy and Direction

The Second Law: Entropy and Direction Concepts

The First Law says energy is conserved, but it doesn't restrict the direction of energy transfer. The Second Law dictates that direction. There are several equivalent statements of the Second Law:

  • Clausius Statement: Heat can never pass spontaneously from a colder body to a warmer body.
  • Kelvin-Planck Statement: It is impossible to construct a heat engine that, operating in a cycle, extracts heat from a single reservoir and converts it entirely into work. Some heat must be expelled to a colder sink. (No engine is 100% efficient).
  • Entropy Statement: The total entropy (SS) of an isolated system can never decrease over time. ΔStotal0\Delta S_{total} \ge 0.

Entropy (SS)

A measure of the disorder, randomness, or the number of microscopic configurations that correspond to a macroscopic state. In thermodynamics, ΔS=(dQrev/T)\Delta S = \int (dQ_{rev}/T). The Second Law states that natural processes always move towards a state of greater disorder.

Heat Engines and Efficiency

Heat Engines and Efficiency Concepts

A heat engine is a device that extracts heat (QHQ_H) from a hot reservoir, uses some of it to do useful work (WW), and exhausts the remaining waste heat (QCQ_C) to a cold reservoir.

By the First Law, W=QHQCW = Q_H - |Q_C|.

The thermal efficiency (ee) is the ratio of what you get to what you pay for:

Thermal Efficiency of a Heat Engine

Calculates the efficiency of a heat engine based on work output and heat input.

e=WQH=1QCQHe = \frac{W}{Q_H} = 1 - \frac{|Q_C|}{Q_H}

Variables

SymbolDescriptionUnit
eeThermal efficiencydimensionless
WWUseful work done by the engineJ
QHQ_HHeat extracted from the hot reservoirJ
QCQ_CHeat exhausted to the cold reservoirJ

Heat Engines and Efficiency Concepts

The Carnot Engine is an idealized, reversible engine that sets the maximum possible theoretical efficiency between two temperatures:

Carnot Efficiency

Sets the maximum theoretical efficiency for any heat engine operating between two temperatures.

eCarnot=1TCTHe_{Carnot} = 1 - \frac{T_C}{T_H}

Variables

SymbolDescriptionUnit
eCarnote_{Carnot}Maximum theoretical efficiencydimensionless
TCT_CAbsolute temperature of the cold reservoirK
THT_HAbsolute temperature of the hot reservoirK

The Third Law: Absolute Zero

The Third Law: Absolute Zero Concepts

It is impossible to lower the temperature of any system to absolute zero (0 K) in a finite number of steps. As temperature approaches absolute zero, the entropy of a perfect crystal approaches zero.

The Ideal Gas Law and Kinetic Theory

Macroscopic vs. Microscopic

The Ideal Gas Law (PV=nRTPV = nRT) relates the macroscopic properties of a gas: pressure, volume, temperature, and amount of substance.

The Kinetic Theory of Gases provides the microscopic explanation for these macroscopic properties. It models a gas as a large number of tiny, rapidly moving particles in random, continuous motion, colliding elastically with each other and the container walls. The pressure exerted by a gas is the macroscopic result of billions of microscopic particle collisions against the container.

The Ideal Gas Law

The equation of state for a hypothetical ideal gas.

PV=nRT=NkBTPV = nRT = N k_B T

Interactive Simulation

Use this ideal gas model to see how pressure responds when amount, temperature, or volume changes.

Interactive Physics Simulation

Ideal Gas Piston Simulator

Study thermodynamics using a movable piston chamber. Experience kinetic theory as molecules buzz and collide with boundaries at speeds proportional to temperature.

Gas Species
1.5 mol
300 K
0.03
Governing Formulas
Ideal Gas State Equation
PV=nRT    P=nRTVP \cdot V = n \cdot R \cdot T \implies P = \frac{n R T}{V}
Root-Mean-Square Velocity
vrms=3RTMv_{rms} = \sqrt{\frac{3 R T}{M}}
Thermodynamic cylinder gas chamber showing kinetic gas molecular motionMolecular speed scales as vrms ∝ √T
Pressure (P)
149.65 kPa
Gas Mass Density
1.680 kg/m³
Key Takeaways
  • Temperature (TT) is average microscopic kinetic energy; Heat (QQ) is energy transferred due to a ΔT\Delta T.
  • Heat transfer mechanisms are Conduction (contact), Convection (fluid motion), and Radiation (electromagnetic waves).
  • Specific heat (cc) relates QQ to ΔT\Delta T; Latent heat (LL) relates QQ to phase changes without ΔT\Delta T.
  • Zeroth Law: Defines temperature via thermal equilibrium.
  • First Law: Conservation of energy (ΔU=QW\Delta U = Q - W).
  • Second Law: Dictates the direction of processes (heat flows hot to cold) and introduces Entropy (disorder always increases). No engine is 100% efficient.