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Thermodynamics

Thermodynamics visualizer

A kinetic-theory gas box with real measured pressure, the four classic PV processes, heat engines and the Carnot cycle, calorimetry with latent heat and mixtures, conduction, radiation, Newton's law of cooling, thermal expansion, and the speeds of gas molecules — ten sandboxes with graphs of what is happening and a worked explanation that does the sums with your numbers.

The physics behind it
Formulas used in this lab

Ideal gas and kinetic theory Class 11

Ideal gas law
PV = nRT = NkBT
Pressure from molecular motion
P = (1/3)(N/V) m⟨v²⟩
Average kinetic energy per molecule
½m⟨v²⟩ = (3/2)kBT
rms speed
vrms = √(3kBT/m) = √(3RT/M)
Gas laws
Boyle: PV = const (T fixed); Charles: V/T = const (P fixed); Gay-Lussac: P/T = const (V fixed)
In the box lab
P ∝ NT/V: more particles, a hotter gas or a smaller volume all raise the pressure

First law and the four processes Class 11

First law
Q = ΔU + W,  W = ∫ P dV (area under the PV curve)
Internal energy of an ideal gas
ΔU = nCvΔT,  Cp − Cv = R,  γ = Cp/Cv (1.4 here)
Isothermal (T constant)
PV = const,  ΔU = 0,  W = nRT ln(V2/V1)
Isobaric (P constant)
V/T = const,  W = PΔV
Isochoric (V constant)
P/T = const,  W = 0,  Q = ΔU
Adiabatic (Q = 0)
PVγ = const,  TVγ−1 = const,  W = (P1V1 − P2V2)/(γ − 1)
Adiabatic vs isothermal
the adiabatic curve is steeper on a PV diagram

Heat engines and refrigerators Class 11

Engine
W = Qh − Qc; efficiency η = W/Qh = 1 − Qc/Qh (Qh counts all the heat absorbed)
Work in a cycle
W = area enclosed on the PV diagram; ΔU = 0 over a whole cycle
Carnot cycle
two isotherms and two adiabats; Qc/Qh = Tc/Th; η = 1 − Tc/Th (the maximum possible)
Carnot heats
Qh = nRTh ln(VB/VA), Qc = nRTc ln(VC/VD), with VB/VA = VC/VD
Otto cycle
η = 1 − r1−γ with r the compression ratio
Refrigerator
COP = Qc/W = Tc/(Th − Tc) (Carnot); heat pump COP = Th/(Th − Tc)
Second law
Kelvin–Planck: no engine converts heat entirely into work; Clausius: heat does not flow by itself from cold to hot

Calorimetry Class 11

Heat and temperature change
Q = mcΔT = CΔT (c specific heat, C = mc heat capacity)
Change of state
Q = mL: Lf = 334 kJ/kg (ice), Lv = 2260 kJ/kg (water)
Specific heats (J/kg·K)
water 4186, ice 2100, steam 2010, copper 385, aluminium 900, iron 450
Principle of calorimetry
heat lost = heat gained; Tf = (m1c1T1 + m2c2T2)/(m1c1 + m2c2)
Time to heat
t = Q/P for a heater of power P

Heat transfer Class 11

Conduction
H = Q/t = kAΔT/L; thermal resistance R = L/kA, H = ΔT/R
Series and parallel
series: R = R1 + R2 (same H); parallel: H = H1 + H2 (same ΔT)
Stefan–Boltzmann law
P = εσAT4, σ = 5.67 × 10−8 W/m2K4; net P = εσA(T4 − Ts4)
Wien's displacement law
λmaxT = 2.898 × 10−3 m·K
Newton's law of cooling
dT/dt = −k(T − Ts); T = Ts + (T0 − Ts)e−kt; (T1 − T2)/t = k((T1 + T2)/2 − Ts)
Convection
heat carried by the flow of a fluid; air is a poor conductor but a good convector

Thermal expansion Class 11

Linear
ΔL = αL0ΔT, L = L0(1 + αΔT)
Area and volume
ΔA = βA0ΔT with β = 2α; ΔV = γV0ΔT with γ = 3α
Thermal stress (rod held at both ends)
stress = YαΔT; force = Y A αΔT
Bimetallic strip
R = 2h/[3(α2 − α1)ΔT] for two layers of equal thickness; it bends towards the metal with the smaller α
Water
contracts on heating between 0 and 4 °C; densest at 4 °C

Molecular speeds and heat capacities Class 11

Characteristic speeds
vp = √(2RT/M),  v̄ = √(8RT/πM),  vrms = √(3RT/M); ratio 1 : 1.128 : 1.225
Maxwell distribution
f(v) = 4π(M/2πRT)3/2 v2 e−Mv2/2RT; the area under it between two speeds is the fraction of molecules there
Equipartition
energy ½kBT per degree of freedom; U = (f/2)nRT
Heat capacities
Cv = (f/2)R, Cp = (f/2 + 1)R, γ = 1 + 2/f
Values of f
monatomic 3 (γ = 5/3); diatomic 5 (γ = 7/5); non-linear polyatomic 6 (γ = 4/3)