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Section A: Long Answer Questions

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5 questions
1long10 marks

Set up the differential equation of a damped harmonic oscillator and obtain its solution for the under-damped case. Hence define the relaxation time and quality factor.

A damped oscillator has mass m=0.20kgm = 0.20\,\text{kg}, force constant k=80N/mk = 80\,\text{N/m} and damping constant b=0.40kg/sb = 0.40\,\text{kg/s}. Calculate (i) the angular frequency of the damped oscillation and (ii) the time in which the amplitude falls to 1/e1/e of its initial value.

Differential equation. A particle of mass mm experiences a restoring force kx-kx and a velocity-dependent damping force bdxdt-b\dfrac{dx}{dt}. By Newton's second law:

md2xdt2=kxbdxdtm\frac{d^2x}{dt^2} = -kx - b\frac{dx}{dt} d2xdt2+2βdxdt+ω02x=0,2β=bm,    ω02=km\frac{d^2x}{dt^2} + 2\beta\frac{dx}{dt} + \omega_0^2 x = 0,\qquad 2\beta=\frac{b}{m},\;\; \omega_0^2=\frac{k}{m}

Solution. Trying x=eαtx=e^{\alpha t} gives the auxiliary equation α2+2βα+ω02=0\alpha^2 + 2\beta\alpha + \omega_0^2 = 0, so

α=β±β2ω02\alpha = -\beta \pm \sqrt{\beta^2-\omega_0^2}

For the under-damped case β2<ω02\beta^2<\omega_0^2, write ω=ω02β2\omega = \sqrt{\omega_0^2-\beta^2}. The general solution is

x(t)=A0eβtcos(ωt+ϕ)\boxed{x(t) = A_0\,e^{-\beta t}\cos(\omega t + \phi)}

This is an oscillation of angular frequency ω\omega whose amplitude A0eβtA_0 e^{-\beta t} decays exponentially.

Relaxation time τ\tau is the time for the amplitude to fall to 1/e1/e of its initial value: eβτ=e1τ=1/β=2m/be^{-\beta\tau}=e^{-1}\Rightarrow \tau = 1/\beta = 2m/b.

Quality factor Q=ω2β=ωτ/2Q = \dfrac{\omega}{2\beta} = \omega\tau/2, measuring how many radians the oscillator swings before its energy decays by 1/e1/e.

Numerical work.

ω02=k/m=80/0.20=400s2\omega_0^2 = k/m = 80/0.20 = 400\,\text{s}^{-2}, so ω0=20rad/s\omega_0 = 20\,\text{rad/s}.

β=b/(2m)=0.40/(2×0.20)=1.0s1\beta = b/(2m) = 0.40/(2\times0.20) = 1.0\,\text{s}^{-1}.

(i) ω=ω02β2=4001=399=19.975rad/s\omega = \sqrt{\omega_0^2-\beta^2} = \sqrt{400-1} = \sqrt{399} = 19.975\,\text{rad/s}.

ω19.97rad/s\omega \approx 19.97\,\text{rad/s}

(ii) τ=1/β=1/1.0=1.0s\tau = 1/\beta = 1/1.0 = 1.0\,\text{s}.

Amplitude falls to 1/e1/e in τ=1.0s\tau = 1.0\,\text{s}.

oscillationsdamped-oscillationdifferential-equation
2long10 marks

Describe the formation of Newton's rings by reflected light and derive an expression for the diameter of the nnth dark ring. Explain why the centre appears dark.

In a Newton's rings experiment the diameter of the 10th dark ring is 5.0mm5.0\,\text{mm} and that of the 20th dark ring is 7.0mm7.0\,\text{mm}. The plano-convex lens is illuminated normally with light of wavelength 589nm589\,\text{nm}. Find the radius of curvature of the lower surface of the lens.

Formation. A plano-convex lens of large radius of curvature RR rests on a flat glass plate, enclosing a thin air film of variable thickness tt. Monochromatic light incident normally is partly reflected at the top of the air film and partly at the bottom; the two reflected beams interfere, producing concentric bright and dark rings (loci of constant tt) centred on the point of contact.

Condition for dark rings (reflected light). The path difference is 2t+λ/22t + \lambda/2 (the extra λ/2\lambda/2 from the phase reversal at the glass-to-air reflection at the lower surface). For a dark ring,

2t+λ2=(m+12)λ    2t=mλ,m=0,1,2,2t + \frac{\lambda}{2} = \left(m+\tfrac{1}{2}\right)\lambda \;\Rightarrow\; 2t = m\lambda,\quad m=0,1,2,\dots

Geometry of the film: for a ring of radius rr, r2=(2Rt)t2Rtr^2 = (2R-t)t \approx 2Rt (since tRt\ll R), so t=r2/2Rt = r^2/2R. Substituting,

2r22R=mλ    r2=mRλ2\cdot\frac{r^2}{2R} = m\lambda \;\Rightarrow\; r^2 = mR\lambda

With diameter D=2rD=2r:

Dm2=4mRλ\boxed{D_m^2 = 4mR\lambda}

Why the centre is dark. At the point of contact t=0t=0, so the only path difference is the λ/2\lambda/2 phase change at the lower reflection: the two beams are exactly out of phase and interfere destructively. Hence the centre is dark.

Numerical work. Using two rings eliminates uncertainty in the contact point:

D202D102=4Rλ(2010)=40RλD_{20}^2 - D_{10}^2 = 4R\lambda(20-10) = 40R\lambda

D202=(7.0×103)2=49.0×106m2D_{20}^2 = (7.0\times10^{-3})^2 = 49.0\times10^{-6}\,\text{m}^2

D102=(5.0×103)2=25.0×106m2D_{10}^2 = (5.0\times10^{-3})^2 = 25.0\times10^{-6}\,\text{m}^2

D202D102=24.0×106m2D_{20}^2 - D_{10}^2 = 24.0\times10^{-6}\,\text{m}^2

R=D202D10240λ=24.0×10640×589×109=24.0×1062.356×105R = \frac{D_{20}^2-D_{10}^2}{40\lambda} = \frac{24.0\times10^{-6}}{40\times589\times10^{-9}} = \frac{24.0\times10^{-6}}{2.356\times10^{-5}} R=1.0187mR = 1.0187\,\text{m}

Radius of curvature R1.02mR \approx 1.02\,\text{m}.

physical-opticsnewtons-ringsinterference
3long8 marks

State Maxwell's four equations in differential form and explain the physical significance of each. Starting from these equations, show that electromagnetic waves propagate through free space with speed c=1/μ0ε0c = 1/\sqrt{\mu_0\varepsilon_0}, and evaluate cc numerically.

Maxwell's equations (differential form, free space with sources).

  1. E=ρε0\nabla\cdot\vec{E} = \dfrac{\rho}{\varepsilon_0} — Gauss's law: electric charge is the source of the electric field (field lines begin/end on charge).
  2. B=0\nabla\cdot\vec{B} = 0 — no magnetic monopoles; magnetic field lines are closed loops.
  3. ×E=Bt\nabla\times\vec{E} = -\dfrac{\partial \vec{B}}{\partial t} — Faraday's law: a time-varying magnetic field induces a circulating electric field.
  4. ×B=μ0J+μ0ε0Et\nabla\times\vec{B} = \mu_0\vec{J} + \mu_0\varepsilon_0\dfrac{\partial \vec{E}}{\partial t} — Ampere-Maxwell law: both conduction current and displacement current produce a magnetic field.

Wave equation in free space (ρ=0,  J=0\rho=0,\;\vec{J}=0). Take the curl of equation 3:

×(×E)=t(×B)\nabla\times(\nabla\times\vec{E}) = -\frac{\partial}{\partial t}(\nabla\times\vec{B})

Use the identity ×(×E)=(E)2E\nabla\times(\nabla\times\vec{E}) = \nabla(\nabla\cdot\vec{E}) - \nabla^2\vec{E}. With E=0\nabla\cdot\vec{E}=0 and substituting equation 4 (with J=0\vec{J}=0):

2E=t(μ0ε0Et)-\nabla^2\vec{E} = -\frac{\partial}{\partial t}\left(\mu_0\varepsilon_0\frac{\partial\vec{E}}{\partial t}\right) 2E=μ0ε02Et2\boxed{\nabla^2\vec{E} = \mu_0\varepsilon_0\frac{\partial^2\vec{E}}{\partial t^2}}

This is the wave equation 2E=1v22Et2\nabla^2\vec{E} = \dfrac{1}{v^2}\dfrac{\partial^2\vec{E}}{\partial t^2} with propagation speed

v=c=1μ0ε0v = c = \frac{1}{\sqrt{\mu_0\varepsilon_0}}

An identical equation holds for B\vec{B}.

Numerical value.

μ0=4π×107T\cdotpm/A=1.2566×106\mu_0 = 4\pi\times10^{-7}\,\text{T·m/A} = 1.2566\times10^{-6}, ε0=8.854×1012F/m\varepsilon_0 = 8.854\times10^{-12}\,\text{F/m}.

μ0ε0=1.2566×106×8.854×1012=1.1127×1017s2/m2\mu_0\varepsilon_0 = 1.2566\times10^{-6}\times8.854\times10^{-12} = 1.1127\times10^{-17}\,\text{s}^2/\text{m}^2.

c=11.1127×1017=13.336×109=2.998×108m/sc = \frac{1}{\sqrt{1.1127\times10^{-17}}} = \frac{1}{3.336\times10^{-9}} = 2.998\times10^{8}\,\text{m/s}

c3.0×108m/sc \approx 3.0\times10^{8}\,\text{m/s}, equal to the measured speed of light, identifying light as an electromagnetic wave.

electromagnetismmaxwell-equationsem-waves
4long8 marks

Set up the time-independent Schrödinger equation for a particle confined in a one-dimensional infinite potential well of width LL. Obtain the normalized eigenfunctions and the energy eigenvalues.

Calculate the energy (in eV) of the lowest two states of an electron confined in a well of width L=0.10nmL = 0.10\,\text{nm}.

Setup. Inside the well (0<x<L0<x<L) the potential V=0V=0; outside, V=V=\infty so ψ=0\psi=0. The time-independent Schrödinger equation inside is

22md2ψdx2=Eψ    d2ψdx2+k2ψ=0,k2=2mE2-\frac{\hbar^2}{2m}\frac{d^2\psi}{dx^2} = E\psi \;\Rightarrow\; \frac{d^2\psi}{dx^2} + k^2\psi = 0,\quad k^2 = \frac{2mE}{\hbar^2}

General solution and boundary conditions. ψ(x)=Asinkx+Bcoskx\psi(x)=A\sin kx + B\cos kx. The wavefunction must vanish at the walls:

  • ψ(0)=0B=0\psi(0)=0 \Rightarrow B=0.
  • ψ(L)=0AsinkL=0kL=nπ,  n=1,2,3,\psi(L)=0 \Rightarrow A\sin kL=0 \Rightarrow kL = n\pi,\; n=1,2,3,\dots

Thus kn=nπ/Lk_n = n\pi/L and ψn(x)=AsinnπxL\psi_n(x)=A\sin\dfrac{n\pi x}{L}.

Normalization. 0LA2sin2nπxLdx=A2L2=1A=2/L\displaystyle\int_0^L A^2\sin^2\frac{n\pi x}{L}\,dx = A^2\frac{L}{2}=1 \Rightarrow A=\sqrt{2/L}.

ψn(x)=2LsinnπxL\boxed{\psi_n(x)=\sqrt{\frac{2}{L}}\sin\frac{n\pi x}{L}}

Energy eigenvalues. From kn2=2mEn/2k_n^2 = 2mE_n/\hbar^2:

En=n2π222mL2=n2h28mL2\boxed{E_n = \frac{n^2\pi^2\hbar^2}{2mL^2} = \frac{n^2 h^2}{8mL^2}}

Numerical work (m=9.11×1031kgm=9.11\times10^{-31}\,\text{kg}, h=6.626×1034J\cdotpsh=6.626\times10^{-34}\,\text{J·s}, L=0.10×109mL=0.10\times10^{-9}\,\text{m}):

E1=h28mL2=(6.626×1034)28×9.11×1031×(1.0×1010)2E_1 = \frac{h^2}{8mL^2} = \frac{(6.626\times10^{-34})^2}{8\times9.11\times10^{-31}\times(1.0\times10^{-10})^2}

Numerator: (6.626×1034)2=4.390×1067(6.626\times10^{-34})^2 = 4.390\times10^{-67}.

Denominator: 8×9.11×1031×1.0×1020=7.288×10508\times9.11\times10^{-31}\times1.0\times10^{-20} = 7.288\times10^{-50}.

E1=4.390×10677.288×1050=6.024×1018JE_1 = \frac{4.390\times10^{-67}}{7.288\times10^{-50}} = 6.024\times10^{-18}\,\text{J}

Convert: E1=6.024×10181.602×1019=37.6eVE_1 = \dfrac{6.024\times10^{-18}}{1.602\times10^{-19}} = 37.6\,\text{eV}.

E2=4E1=4×37.6=150.4eVE_2 = 4E_1 = 4\times37.6 = 150.4\,\text{eV}.

E137.6eVE_1 \approx 37.6\,\text{eV},   E2150.4eV\;E_2 \approx 150.4\,\text{eV}.

quantum-mechanicsschrodinger-equationparticle-in-box
5long9 marks

Define electric capacitance. Derive an expression for the capacitance of a parallel-plate capacitor partially filled with a dielectric slab of thickness tt (slab thickness less than plate separation dd) and dielectric constant KK.

A parallel-plate capacitor has plate area A=200cm2A = 200\,\text{cm}^2 and plate separation d=4.0mmd = 4.0\,\text{mm}. A dielectric slab of thickness t=3.0mmt = 3.0\,\text{mm} and dielectric constant K=5K = 5 is inserted. Find the capacitance.

Capacitance is the charge stored per unit potential difference: C=Q/VC = Q/V. Its SI unit is the farad (F).

Derivation (partially filled). Let surface charge density on the plates be σ=Q/A\sigma = Q/A. The free-space field between bare plates is E0=σ/ε0E_0 = \sigma/\varepsilon_0; inside the dielectric the field is reduced to E=E0/K=σ/(Kε0)E = E_0/K = \sigma/(K\varepsilon_0).

The potential difference is the sum of contributions across the air gap (dt)(d-t) and the dielectric (t)(t):

V=E0(dt)+Et=σε0(dt)+σKε0t=σε0[(dt)+tK]V = E_0(d-t) + E\,t = \frac{\sigma}{\varepsilon_0}(d-t) + \frac{\sigma}{K\varepsilon_0}t = \frac{\sigma}{\varepsilon_0}\left[(d-t)+\frac{t}{K}\right]

Since σ=Q/A\sigma = Q/A,

C=QV=QQAε0[(dt)+tK]C = \frac{Q}{V} = \frac{Q}{\frac{Q}{A\varepsilon_0}\left[(d-t)+\frac{t}{K}\right]} C=ε0A(dt)+tK\boxed{C = \frac{\varepsilon_0 A}{(d-t)+\dfrac{t}{K}}}

Numerical work. A=200cm2=200×104=2.0×102m2A = 200\,\text{cm}^2 = 200\times10^{-4} = 2.0\times10^{-2}\,\text{m}^2; d=4.0×103md = 4.0\times10^{-3}\,\text{m}; t=3.0×103mt = 3.0\times10^{-3}\,\text{m}; K=5K=5; ε0=8.854×1012F/m\varepsilon_0 = 8.854\times10^{-12}\,\text{F/m}.

Effective gap: (dt)+t/K=(4.03.0)×103+3.0×1035=1.0×103+0.6×103=1.6×103m(d-t) + t/K = (4.0-3.0)\times10^{-3} + \dfrac{3.0\times10^{-3}}{5} = 1.0\times10^{-3} + 0.6\times10^{-3} = 1.6\times10^{-3}\,\text{m}.

C=8.854×1012×2.0×1021.6×103=1.7708×10131.6×103=1.107×1010FC = \frac{8.854\times10^{-12}\times2.0\times10^{-2}}{1.6\times10^{-3}} = \frac{1.7708\times10^{-13}}{1.6\times10^{-3}} = 1.107\times10^{-10}\,\text{F}

C110.7pFC \approx 110.7\,\text{pF} (about 0.111nF0.111\,\text{nF}).

electrostaticscapacitordielectrics
B

Section B: Short Answer Questions

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6 questions
6short6 marks

State Sabine's reverberation formula and define reverberation time. A hall of volume 1500m31500\,\text{m}^3 has a total absorption of 120m2120\,\text{m}^2 sabine (open-window units). Calculate its reverberation time. If carpets adding 30m230\,\text{m}^2 of absorption are introduced, what is the new reverberation time?

Reverberation time TT is the time taken for the steady-state sound intensity in a room to fall to 10610^{-6} of its original value (a drop of 60 dB) after the source stops.

Sabine's formula:

T=0.161VAT = \frac{0.161\,V}{A}

where VV is the room volume in m3\text{m}^3 and A=aiSiA=\sum a_i S_i is the total absorption in metric sabine (m²).

Case 1.

T1=0.161×1500120=241.5120=2.0125sT_1 = \frac{0.161\times1500}{120} = \frac{241.5}{120} = 2.0125\,\text{s}

T12.01sT_1 \approx 2.01\,\text{s}.

Case 2. New total absorption A2=120+30=150m2A_2 = 120 + 30 = 150\,\text{m}^2.

T2=0.161×1500150=241.5150=1.61sT_2 = \frac{0.161\times1500}{150} = \frac{241.5}{150} = 1.61\,\text{s}

T2=1.61sT_2 = 1.61\,\text{s} — adding absorption shortens the reverberation time, improving speech clarity.

acousticsreverberationsabine-formula
7short6 marks

Explain how a plane diffraction grating produces principal maxima and write the grating equation. A grating has 5000 lines per cm. Find the angle of diffraction for the second-order principal maximum of light of wavelength 546nm546\,\text{nm}.

Principal maxima. A grating is a large number NN of equally spaced parallel slits of spacing dd (grating element). When a plane wave is incident normally, light from adjacent slits has a path difference dsinθd\sin\theta. Whenever this equals a whole number of wavelengths, the contributions from all slits add in phase, giving a sharp, intense principal maximum:

dsinθ=nλ,n=0,1,2,\boxed{d\sin\theta = n\lambda},\qquad n=0,1,2,\dots

Numerical work. Grating element:

d=1cm5000=1×1025000=2.0×106md = \frac{1\,\text{cm}}{5000} = \frac{1\times10^{-2}}{5000} = 2.0\times10^{-6}\,\text{m}

For n=2n=2, λ=546×109m\lambda = 546\times10^{-9}\,\text{m}:

sinθ=nλd=2×546×1092.0×106=1.092×1062.0×106=0.546\sin\theta = \frac{n\lambda}{d} = \frac{2\times546\times10^{-9}}{2.0\times10^{-6}} = \frac{1.092\times10^{-6}}{2.0\times10^{-6}} = 0.546 θ=sin1(0.546)=33.09\theta = \sin^{-1}(0.546) = 33.09^\circ

θ33.1\theta \approx 33.1^\circ.

physical-opticsdiffraction-gratingresolving-power
8short5 marks

Define acceptance angle and numerical aperture of a step-index optical fibre. A fibre has core refractive index n1=1.50n_1 = 1.50 and cladding index n2=1.46n_2 = 1.46. Calculate its numerical aperture and acceptance angle (in air).

Acceptance angle θa\theta_a is the maximum half-angle of the cone of light (measured from the fibre axis) that can enter the core and still undergo total internal reflection, so that it is guided along the fibre.

Numerical aperture (NA) is the sine of the acceptance angle; it measures the light-gathering capacity of the fibre:

NA=sinθa=n12n22\text{NA} = \sin\theta_a = \sqrt{n_1^2 - n_2^2}

(for a fibre in air, where the outer medium n0=1n_0=1).

Numerical work.

n12=1.502=2.2500n_1^2 = 1.50^2 = 2.2500

n22=1.462=2.1316n_2^2 = 1.46^2 = 2.1316

n12n22=2.25002.1316=0.1184n_1^2 - n_2^2 = 2.2500 - 2.1316 = 0.1184

NA=0.1184=0.3441\text{NA} = \sqrt{0.1184} = 0.3441

NA 0.344\approx 0.344.

Acceptance angle:

θa=sin1(0.3441)=20.13\theta_a = \sin^{-1}(0.3441) = 20.13^\circ

θa20.1\theta_a \approx 20.1^\circ.

fiber-opticsnumerical-aperturetotal-internal-reflection
9short6 marks

State the Biot–Savart law. Using it, derive the magnetic field at the centre of a circular current loop of radius RR carrying current II. Calculate the field at the centre of a loop of radius 5.0cm5.0\,\text{cm} carrying 3.0A3.0\,\text{A}.

Biot–Savart law. A current element IdlI\,d\vec{l} produces, at a point with position vector r\vec{r} from the element, a magnetic field

dB=μ04πIdl×r^r2d\vec{B} = \frac{\mu_0}{4\pi}\frac{I\,d\vec{l}\times\hat{r}}{r^2}

directed perpendicular to both dld\vec{l} and r\vec{r}.

Field at the centre of a circular loop. For every element, dlrd\vec{l}\perp\vec{r} (so dl×r^=dl|d\vec{l}\times\hat{r}| = dl) and r=Rr=R. All elements give dBd\vec{B} in the same direction (along the axis through the centre), so magnitudes add:

B=dB=μ0I4πR202πRdl=μ0I4πR2(2πR)B = \int dB = \frac{\mu_0 I}{4\pi R^2}\int_0^{2\pi R} dl = \frac{\mu_0 I}{4\pi R^2}(2\pi R) B=μ0I2R\boxed{B = \frac{\mu_0 I}{2R}}

Numerical work. μ0=4π×107T\cdotpm/A\mu_0 = 4\pi\times10^{-7}\,\text{T·m/A}, I=3.0AI = 3.0\,\text{A}, R=5.0×102mR = 5.0\times10^{-2}\,\text{m}.

B=4π×107×3.02×5.0×102=1.2566×106×3.00.10=3.770×1060.10B = \frac{4\pi\times10^{-7}\times3.0}{2\times5.0\times10^{-2}} = \frac{1.2566\times10^{-6}\times3.0}{0.10} = \frac{3.770\times10^{-6}}{0.10} B=3.770×105TB = 3.770\times10^{-5}\,\text{T}

B3.77×105T=37.7μTB \approx 3.77\times10^{-5}\,\text{T} = 37.7\,\mu\text{T}.

electromagnetismbiot-savartmagnetic-field
10short6 marks

Distinguish between spontaneous and stimulated emission. Explain what is meant by population inversion and why it is essential for laser action. State the role of the metastable state.

Spontaneous emission. An atom in an excited state E2E_2 decays to a lower state E1E_1 on its own, after a random time, emitting a photon of energy hν=E2E1h\nu = E_2 - E_1. The emitted photons are random in direction, phase and polarization, so the light is incoherent (ordinary light sources).

Stimulated emission. An incident photon of energy exactly hν=E2E1h\nu = E_2 - E_1 induces an excited atom to drop to E1E_1, emitting a second photon. This emitted photon is identical to the incident one — same frequency, phase, direction and polarization. The two coherent photons can then stimulate further emissions, giving the multiplication (light amplification) at the heart of a laser.

FeatureSpontaneousStimulated
Triggernone (random)incident photon
Phase/directionrandomidentical to incident
Coherenceincoherentcoherent

Population inversion. In thermal equilibrium more atoms occupy the lower state (N1>N2N_1 > N_2, Boltzmann distribution), so absorption dominates over stimulated emission. Population inversion is the non-equilibrium condition N2>N1N_2 > N_1, achieved by pumping. Only then does an incident beam gain more photons by stimulated emission than it loses by absorption, so net light amplification — laser action — becomes possible. Hence population inversion is the essential prerequisite for lasing.

Role of the metastable state. A metastable level has an unusually long lifetime (microseconds to milliseconds) compared with ordinary excited states (nanoseconds). Atoms pumped to a higher level decay quickly into the metastable state and accumulate there, allowing N2N_2 to build up above N1N_1. Without a metastable state, atoms would de-excite too fast for population inversion to be sustained.

lasersstimulated-emissionpopulation-inversion
11short6 marks

What is the Meissner effect? Distinguish between Type I and Type II superconductors. Also state, with a brief reason, how the electrical conductivity of an intrinsic semiconductor changes with rising temperature.

Meissner effect. When a material is cooled below its critical temperature TcT_c in a magnetic field, it expels the magnetic flux from its interior, so that B=0\vec{B}=0 inside the bulk. A superconductor is therefore a perfect diamagnet (χ=1\chi = -1), not merely a perfect conductor; the flux is pushed out even if the field was applied before cooling.

Type I vs Type II superconductors.

FeatureType IType II
Critical fieldssingle HcH_ctwo: Hc1H_{c1} and Hc2H_{c2}
Transitionabrupt loss of superconductivity at HcH_cgradual; mixed (vortex) state between Hc1H_{c1} and Hc2H_{c2}
Meissner effectcomplete up to HcH_ccomplete up to Hc1H_{c1}, partial above
Examplespure metals (Hg, Pb, Sn)alloys, Nb–Ti, Nb₃Sn, ceramics
Uselow-fieldhigh-field magnets

Intrinsic semiconductor conductivity vs temperature. The electrical conductivity increases as temperature rises. Reason: thermal energy excites more electrons across the band gap from the valence band to the conduction band, generating additional electron–hole pairs. The carrier concentration grows roughly as neEg/2kBTn \propto e^{-E_g/2k_BT}, and this rapid exponential rise in carrier number outweighs the small fall in mobility, so σ\sigma increases — opposite to the behaviour of metals.

superconductivitymeissner-effectsemiconductors

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