ThermodynamicsTopic #20 of 35

First Law of Thermodynamics

Internal energy, work, heat, and conservation of energy in thermal systems.

Overview

The first law of thermodynamics is a statement of energy conservation for thermal systems. It relates heat, work, and internal energy.

Statement

ΔU=QW\Delta U = Q - W

Or equivalently:

Q=ΔU+WQ = \Delta U + W

Where:

  • ΔU\Delta U = change in internal energy
  • QQ = heat added to the system
  • WW = work done BY the system

Sign Conventions

QuantityPositiveNegative
QQHeat absorbedHeat released
WWWork done by systemWork done on system
ΔU\Delta UEnergy increasesEnergy decreases

Internal Energy

  • Total kinetic and potential energy of molecules
  • Depends only on temperature (for ideal gas)
  • State function (path independent)

For ideal monatomic gas:

U=32nRTU = \frac{3}{2}nRT

For ideal diatomic gas:

U=52nRTU = \frac{5}{2}nRT

Change in internal energy:

ΔU=nCvΔT\Delta U = nC_v\Delta T

Work Done by a Gas

General Expression

W=PdVW = \int P \, dV

Work equals area under P-V curve

Constant Pressure (Isobaric)

W=PΔV=P(V2V1)W = P\Delta V = P(V_2 - V_1)

Constant Volume (Isochoric)

W=0W = 0

Isothermal (Constant Temperature)

W=nRTln(V2V1)=nRTln(P1P2)W = nRT \ln\left(\frac{V_2}{V_1}\right) = nRT \ln\left(\frac{P_1}{P_2}\right)

Adiabatic (No Heat Transfer)

W=P1V1P2V2γ1=nCv(T1T2)W = \frac{P_1V_1 - P_2V_2}{\gamma - 1} = nC_v(T_1 - T_2)

Thermodynamic Processes

Isothermal Process (ΔT=0\Delta T = 0)

  • Temperature constant
  • ΔU=0\Delta U = 0
  • Q=WQ = W
  • PV=constantPV = \text{constant}

Isobaric Process (ΔP=0\Delta P = 0)

  • Pressure constant
  • W=PΔVW = P\Delta V
  • Q=nCpΔTQ = nC_p\Delta T

Isochoric Process (ΔV=0\Delta V = 0)

  • Volume constant
  • W=0W = 0
  • Q=ΔU=nCvΔTQ = \Delta U = nC_v\Delta T

Adiabatic Process (Q=0Q = 0)

  • No heat exchange
  • ΔU=W\Delta U = -W
  • PVγ=constantPV^\gamma = \text{constant}
  • TVγ1=constantTV^{\gamma-1} = \text{constant}

Heat Capacities of Gases

At Constant Volume

Cv=f2RC_v = \frac{f}{2}R

At Constant Pressure

Cp=Cv+R=f+22RC_p = C_v + R = \frac{f+2}{2}R

Where ff = degrees of freedom:

  • Monatomic: f=3f = 3, Cv=32RC_v = \frac{3}{2}R, Cp=52RC_p = \frac{5}{2}R
  • Diatomic: f=5f = 5, Cv=52RC_v = \frac{5}{2}R, Cp=72RC_p = \frac{7}{2}R

Ratio of Heat Capacities

γ=CpCv=f+2f\gamma = \frac{C_p}{C_v} = \frac{f+2}{f}
  • Monatomic: γ=531.67\gamma = \frac{5}{3} \approx 1.67
  • Diatomic: γ=75=1.4\gamma = \frac{7}{5} = 1.4

Adiabatic Relations

PVγ=constantPV^\gamma = \text{constant} TVγ1=constantTV^{\gamma-1} = \text{constant} TγP1γ=constantT^\gamma P^{1-\gamma} = \text{constant}

Examples

Example 1: Isochoric Heating

2 moles of monatomic gas at 300 K is heated at constant volume to 500 K.

ΔU=nCvΔT=2×32×8.314×200=4988 J\Delta U = nC_v\Delta T = 2 \times \frac{3}{2} \times 8.314 \times 200 = 4988 \text{ J} W=0(constant volume)W = 0 \quad \text{(constant volume)} Q=ΔU=4988 JQ = \Delta U = 4988 \text{ J}

Example 2: Isobaric Expansion

2 moles of diatomic gas expands at 1 atm from 300 K to 400 K.

ΔV=nRΔTP=2×8.314×100101325=0.0164 m3\Delta V = \frac{nR\Delta T}{P} = \frac{2 \times 8.314 \times 100}{101325} = 0.0164 \text{ m}^3 W=PΔV=101325×0.0164=1663 JW = P\Delta V = 101325 \times 0.0164 = 1663 \text{ J} ΔU=nCvΔT=2×52×8.314×100=4157 J\Delta U = nC_v\Delta T = 2 \times \frac{5}{2} \times 8.314 \times 100 = 4157 \text{ J} Q=ΔU+W=5820 JQ = \Delta U + W = 5820 \text{ J}

Example 3: Isothermal Expansion

1 mole of gas at 300 K expands from 1 L to 3 L isothermally.

W=nRTln(V2V1)=1×8.314×300×ln(3)=2740 JW = nRT \ln\left(\frac{V_2}{V_1}\right) = 1 \times 8.314 \times 300 \times \ln(3) = 2740 \text{ J} ΔU=0(isothermal)\Delta U = 0 \quad \text{(isothermal)} Q=W=2740 JQ = W = 2740 \text{ J}

Example 4: Adiabatic Compression

Monatomic gas (γ=53\gamma = \frac{5}{3}) at 300 K, 1 atm is compressed to 1/8 original volume.

T2=T1(V1V2)γ1=300×82/3=300×4=1200 KT_2 = T_1 \left(\frac{V_1}{V_2}\right)^{\gamma-1} = 300 \times 8^{2/3} = 300 \times 4 = 1200 \text{ K} P2=P1(V1V2)γ=1×85/3=32 atmP_2 = P_1 \left(\frac{V_1}{V_2}\right)^\gamma = 1 \times 8^{5/3} = 32 \text{ atm}

Example 5: Cyclic Process

A gas undergoes a cyclic process. Total heat absorbed is 1000 J.

For a complete cycle:

ΔU=0(returns to initial state)\Delta U = 0 \quad \text{(returns to initial state)} Q=W=1000 J(net work done)Q = W = 1000 \text{ J} \quad \text{(net work done)}

Free Expansion

Gas expands into vacuum:

  • W=0W = 0 (no external pressure)
  • Q=0Q = 0 (too fast for heat transfer)
  • ΔU=0\Delta U = 0
  • For ideal gas: ΔT=0\Delta T = 0