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London theory relates a supercurrent to the gauge-invariant momentum of a phase-coherent charged fluid. In its simplest form it predicts magnetic screening over a penetration depth λL\lambda_L. The theory assumes local, linear response and a nearly fixed order-parameter amplitude; it does not determine the pairing mechanism or resolve a vortex core.

The central distinction is between perfect conductivity, which can preserve an initially trapped magnetic field, and the equilibrium Meissner response, which screens a weak applied field. Geometry matters: a thin slab admits substantial field, while a ring can carry a quantized fluxoid without containing an integer number of magnetic flux quanta.

Required background. Classical Electromagnetism supplies Maxwell boundary conditions; Minimal Coupling in Wave Mechanics supplies the signed-charge momentum. Helpful background. Gauge Transformations explains the compensating phase and potential changes.

Superfluid density and London electrodynamics

Section titled “Superfluid density and London electrodynamics”

Use SI units and a nonmagnetic background, so the magnetic-field energy is B2/(2μ0)B^2/(2\mu_0). Let q∗q^\ast be the signed charge of the coherent object, m∗m^\ast its inertial parameter, and nsn_s its density in that convention. For Cooper pairs, q∗=−2eq^\ast=-2e with e>0e>0. Pair density, pair mass and pair charge must be used together. Counting superconducting electrons instead gives the same electromagnetic stiffness only when all three quantities are converted consistently.

Define

Ds=ns(q∗)2m∗,λL−2=μ0Ds.D_s=\frac{n_s(q^\ast)^2}{m^\ast}, \qquad \lambda_L^{-2}=\mu_0D_s.

In a crystal, DsD_s is a response coefficient, generally a tensor. It need not equal the total carrier density times the bare charge-to-mass combination. A measured penetration depth therefore measures stiffness; it is not a model-independent count of paired electrons.

Writing a coarse-grained field as Ψ=nseiθ\Psi=\sqrt{n_s}e^{i\theta} is a convenient normalization of this phenomenological model. It does not identify its amplitude with the largest eigenvalue of a microscopic density matrix. Off-Diagonal Long-Range Order explains that separate coherence diagnostic.

Minimal coupling gives

ps=ℏ∇θ−q∗A,js=nsq∗m∗ps.\begin{aligned} \mathbf p_s&=\hbar\boldsymbol\nabla\theta-q^\ast\mathbf A,\\ \mathbf j_s&=\frac{n_sq^\ast}{m^\ast}\mathbf p_s. \end{aligned}

Under A↦A+∇χ\mathbf A\mapsto\mathbf A+\boldsymbol\nabla\chi and θ↦θ+q∗χ/ℏ\theta\mapsto\theta+q^\ast\chi/\hbar, the two added gradients cancel in ps\mathbf p_s. The current is gauge invariant. The abbreviated relation js=−DsA\mathbf j_s=-D_s\mathbf A requires a compatible constant-phase choice; it is not the general constitutive law.

For uniform scalar stiffness, the London free energy is

FL=Fmatter+FB,Fmatter=∫d3r ns∣ps∣22m∗,FB=∫d3r ∣B∣22μ0.\begin{aligned} F_L&=F_{\rm matter}+F_B,\\ F_{\rm matter}&=\int d^3r\,\frac{n_s|\mathbf p_s|^2}{2m^\ast},\\ F_B&=\int d^3r\,\frac{|\mathbf B|^2}{2\mu_0}. \end{aligned}

Varying the matter term with respect to A\mathbf A gives −js-\mathbf j_s. Varying the entire functional instead gives

δFLδA=−js+∇×Bμ0.\frac{\delta F_L}{\delta\mathbf A} =-\mathbf j_s+\frac{\boldsymbol\nabla\times\mathbf B}{\mu_0}.

Its stationarity is magnetostatic Ampère law, with the external field imposed through boundary conditions. It does not require the screening current to vanish.

Away from vortices, ∇×∇θ=0\boldsymbol\nabla\times\boldsymbol\nabla\theta=0. Taking the curl of the current gives the second London equation:

∇×js=−DsB.\boldsymbol\nabla\times\mathbf j_s=-D_s\mathbf B.

The first London equation, ∂tjs=DsE\partial_t\mathbf j_s=D_s\mathbf E, describes acceleration in the uniform transverse response, with fixed stiffness and no additional electrochemical-potential gradient. A general longitudinal problem also needs phase dynamics, compressibility and charge conservation. Integrating the first equation with Faraday’s law leaves a history-dependent integration constant; the second equation selects the Meissner relation.

Combining ∇×B=μ0js\boldsymbol\nabla\times\mathbf B=\mu_0\mathbf j_s with the second London equation and ∇⋅B=0\boldsymbol\nabla\cdot\mathbf B=0 yields

∇2B=BλL2.\nabla^2\mathbf B=\frac{\mathbf B}{\lambda_L^2}.

For a superconductor in x>0x>0 with a parallel boundary field Bz(0)=B0B_z(0)=B_0, boundedness at large xx selects

Bz(x)=B0e−x/λL,js,y(x)=−1μ0dBzdx,=B0e−x/λLμ0λL,Ky=∫0∞js,y(x) dx=B0μ0.\begin{aligned} B_z(x)&=B_0e^{-x/\lambda_L},\\ j_{s,y}(x)&=-\frac{1}{\mu_0}\frac{dB_z}{dx},\\ &=\frac{B_0e^{-x/\lambda_L}}{\mu_0\lambda_L},\\ K_y&=\int_0^\infty j_{s,y}(x)\,dx =\frac{B_0}{\mu_0}. \end{aligned}

The surface current of elementary magnetostatics is distributed over a finite layer. Its kinetic energy density μ0λL2js2/2\mu_0\lambda_L^2j_s^2/2 equals the magnetic energy density B2/(2μ0)B^2/(2\mu_0) point by point in this ideal solution.

For −d/2≤x≤d/2-d/2\le x\le d/2, with equal parallel fields BaB_a at the faces, reflection symmetry selects a cosh profile:

Bz(x)Ba=cosh⁡(x/λL)cosh⁡[d/(2λL)],⟨Bz⟩Ba=2λLdtanh⁡d2λL.\begin{aligned} \frac{B_z(x)}{B_a} &=\frac{\cosh(x/\lambda_L)}{\cosh[d/(2\lambda_L)]},\\ \frac{\langle B_z\rangle}{B_a} &=\frac{2\lambda_L}{d}\tanh\frac{d}{2\lambda_L}. \end{aligned}

When d≫λLd\gg\lambda_L, most of the interior is field free. When d≪λLd\ll\lambda_L, nearly all the field penetrates. This weak screening of a parallel field does not imply a vanishing superconducting stiffness.

A reversible Meissner state reaches the same equilibrium configuration whether a weak field is applied before or after cooling. A perfect conductor alone instead preserves initial flux. Real superconductors can retain flux through vortices, pinning or metastable barriers; field history and equilibration must therefore be considered when interpreting a screening measurement.

Along a closed contour where Ψ≠0\Psi\ne0, single-valuedness gives ∮∇θ⋅dℓ=2πw\oint\boldsymbol\nabla\theta\cdot d\boldsymbol\ell=2\pi w, with integer ww. Integrating the momentum relation gives

Φf−Φ=μ0λL2∮js⋅dℓ,Φf=whq∗=nΦ0,\begin{aligned} \Phi_f-\Phi&=\mu_0\lambda_L^2\oint\mathbf j_s\cdot d\boldsymbol\ell,\\ \Phi_f&=w\frac{h}{q^\ast}=n\Phi_0, \end{aligned}

where

Φ=∫SB⋅dS,n=sgn⁡(q∗)w,Φ0=h∣q∗∣.\begin{aligned} \Phi&=\int_{\mathcal S}\mathbf B\cdot d\mathbf S,\\ n&=\operatorname{sgn}(q^\ast)w,\\ \Phi_0&=\frac{h}{|q^\ast|}. \end{aligned}

For Cooper pairs, Φ0=h/(2e)≃2.068×10−15 Wb\Phi_0=h/(2e)\simeq2.068\times10^{-15}\,\mathrm{Wb}. The signed winding ww and positive-quantum integer nn differ by a minus sign for negatively charged pairs.

The fluxoid Φf\Phi_f includes the current term. Flux itself is approximately nΦ0n\Phi_0 only if the contour can be taken deep inside a thick wall where the current is negligible. In a simply connected, nonsingular Meissner region, a loop shrinks to a point and w=0w=0.

For a narrow ring with uniform current across wire area AwA_w and circumference ℓ\ell, define its kinetic inductance

Lk=μ0λL2ℓAw.L_k=\mu_0\lambda_L^2\frac{\ell}{A_w}.

If LgL_g is the geometric inductance and Φext\Phi_{\rm ext} the applied flux, the lumped model gives

Φ=Φext+LgI,Φ+LkI=nΦ0,I=nΦ0−ΦextLg+Lk.\begin{aligned} \Phi&=\Phi_{\rm ext}+L_g I,\\ \Phi+L_kI&=n\Phi_0,\\ I&=\frac{n\Phi_0-\Phi_{\rm ext}}{L_g+L_k}. \end{aligned}

Increasing Lk/LgL_k/L_g allows flux to depart substantially from nΦ0n\Phi_0 while the fluxoid remains quantized. These equations describe a chosen winding branch; a phase slip can change nn. They also require currents below the scale that strongly suppresses the amplitude.

Exact field profiles across superconducting slabs and magnetic flux along one ring winding branch

Geometry changes London screening. Above: slabs with different d/λLd/\lambda_L have the same boundary field but different interior fields. Below: on the fixed n=1n=1 ring branch, Φ/Φ0=(1+rf)/(1+r)\Phi/\Phi_0=(1+r f)/(1+r), where r=Lk/Lgr=L_k/L_g and f=Φext/Φ0f=\Phi_{\rm ext}/\Phi_0. The horizontal curve is the Lk/Lg→0L_k/L_g\to0 limit. The figure does not assume that this branch is the equilibrium state at every applied flux.

For a film with d≪λLd\ll\lambda_L, a perpendicular vortex or a laterally varying field produces currents that are nearly uniform through the thickness, while stray fields spread into the surrounding vacuum. The crossover distance in the plane is

ΛP=2λL2d.\Lambda_P=\frac{2\lambda_L^2}{d}.

Some authors call λL2/d\lambda_L^2/d the Pearl length, so its definition must accompany a number. In Pearl’s thin-film solution, the isolated-vortex sheet current changes from a 1/r1/r dependence for ξ≪r≪ΛP\xi\ll r\ll\Lambda_P to 1/r21/r^2 for r≫ΛPr\gg\Lambda_P. This perpendicular-field geometry differs from the parallel-field slab solved above. See Vortices for core cutoffs and interactions.

Frequency-domain response and dissipative screening

Section titled “Frequency-domain response and dissipative screening”

Use e−iωte^{-i\omega t} time dependence. The causal London conductivity is

σs(ω)=iDsω+i0+,Re⁡σs=πDsδ(ω),Im⁡σs=Ds P1ω.\begin{aligned} \sigma_s(\omega)&=\frac{iD_s}{\omega+i0^+},\\ \operatorname{Re}\sigma_s&=\pi D_s\delta(\omega),\\ \operatorname{Im}\sigma_s&=D_s\,\mathcal P\frac1\omega. \end{aligned}

Here P\mathcal P is the principal value. The reactive pole and zero-frequency absorption weight are two parts of the same causal response. At finite frequency, quasiparticles add a regular conductivity σn\sigma_n; vortex motion can add another response if the sample is not in the Meissner state.

The sign of a complex penetration length must be tied to its decaying field solution. Neglect displacement current and write Bz(x)=B0e−qxB_z(x)=B_0e^{-q x} in x>0x>0. Maxwell’s equations give

q2=−iμ0ωσ,σ=σn+iDsω,q2=λL−2−iμ0ωσn,λ~=q−1,Re⁡q>0.\begin{aligned} q^2&=-i\mu_0\omega\sigma,\\ \sigma&=\sigma_n+\frac{iD_s}{\omega},\\ q^2&=\lambda_L^{-2}-i\mu_0\omega\sigma_n,\\ \widetilde\lambda&=q^{-1},\qquad \operatorname{Re}q>0. \end{aligned}

For positive frequency and real positive σn\sigma_n, this branch has Im⁡λ~>0\operatorname{Im}\widetilde\lambda>0. Defining the surface impedance for these field directions gives

Zs=Ey(0)Hz(0)=qσ,=−iμ0ωλ~,Zs=Rs−iXs.\begin{aligned} Z_s&=\frac{E_y(0)}{H_z(0)}=\frac q\sigma,\\ &=-i\mu_0\omega\widetilde\lambda,\\ Z_s&=R_s-iX_s. \end{aligned}

The dissipated surface power per area is Rs∣Hz(0)∣2/2≥0R_s|H_z(0)|^2/2\ge0. A lossless London fluid has Zs=−iμ0ωλLZ_s=-i\mu_0\omega\lambda_L; an ordinary Ohmic conductor instead has

λ~=1+i2δ,δ=2μ0ωσn,Zs=(1−i)μ0ω2σn.\begin{aligned} \widetilde\lambda&=\frac{1+i}{2}\delta,\\ \delta&=\sqrt{\frac{2}{\mu_0\omega\sigma_n}},\\ Z_s&=(1-i)\sqrt{\frac{\mu_0\omega}{2\sigma_n}}. \end{aligned}

Using e+iωte^{+i\omega t} conjugates these signs. A microwave penetration depth is therefore not automatically the static λL\lambda_L. Terahertz and Infrared Probes connects complex conductivity to measured spectra and missing-area tests.

Penetration depth as a material observable

Section titled “Penetration depth as a material observable”

A useful dimensionless stiffness ratio is rs(T)=λL2(0)/λL2(T)r_s(T)=\lambda_L^2(0)/\lambda_L^2(T). In the clean, local, isotropic, fully gapped weak-coupling limit,

ΔλL(T)λL(0)≃πΔ02kBT e−Δ0/(kBT).\frac{\Delta\lambda_L(T)}{\lambda_L(0)} \simeq\sqrt{\frac{\pi\Delta_0}{2k_{\mathrm B}T}} \,e^{-\Delta_0/(k_{\mathrm B}T)}.

Nodes can give power laws, but the exponent also depends on the current direction and its matrix element near the node. For example, simple clean axial point-node models can give T2T^2 or T4T^4 in different directions; polar line-node models can give TT or T3T^3. Disorder, nonlocality and surface states further change the result. A single fitted power is not a unique identification of gap symmetry (Prozorov and Giannetta, 2006).

For anisotropic local response, replace DsD_s by a tensor D\mathsf D; the inverse squared penetration-depth tensor is μ0D\mu_0\mathsf D. Field direction, current direction and sample shape are needed to solve the screening problem. Independent-band models add band contributions, but general multiband response can also contain interband current terms.

Microwave impedance, resonators, mutual inductance, muon measurements and scanning magnetic probes infer stiffness through different field models. Many determine λ(T)−λ(Tbase)\lambda(T)-\lambda(T_{\rm base}) more accurately than absolute λ(0)\lambda(0). Calibration, demagnetization, trapped vortices and normal-fluid loss must be included before comparing the result with a gap model. Unconventional Superconductivity combines this information with other probes.

If the current samples the vector potential over distances comparable to the field-variation scale, a nonlocal kernel replaces the pointwise law. Schematically,

ji(r)=∫d3r′ Kij(r,r′)ps,j(r′).j_i(\mathbf r)=\int d^3r'\, \mathcal K_{ij}(\mathbf r,\mathbf r')p_{s,j}(\mathbf r').

This is the setting of Pippard electrodynamics. The local limit requires a kernel range small compared with the electromagnetic variation, not merely a low frequency.

Strong currents, pair-breaking surfaces and vortex cores also violate the fixed-amplitude approximation. Ginzburg–Landau Theory introduces amplitude healing and critical scales; BCS Theory connects pairing to microscopic response. London theory can estimate a vortex’s far-field energy and, with additional core information, a lower critical field. Stiffness alone cannot determine the core energy, transition temperature, gap symmetry or type-I/type-II boundary.

Derive the slab profile and its mean field, then obtain the leading small-d/λLd/\lambda_L reduction of the mean field.

Solution

The general solution is B=Ccosh⁡(x/λL)+Dsinh⁡(x/λL)B=C\cosh(x/\lambda_L)+D\sinh(x/\lambda_L). Equal fields at both faces set D=0D=0 and C=Ba/cosh⁡[d/(2λL)]C=B_a/\cosh[d/(2\lambda_L)]. Integrating across the thickness gives the mean displayed above. With a=d/(2λL)a=d/(2\lambda_L),

⟨B⟩Ba=tanh⁡aa=1−a23+O(a4),1−⟨B⟩Ba=d212λL2+O(d4/λL4).\begin{aligned} \frac{\langle B\rangle}{B_a}&=\frac{\tanh a}{a} =1-\frac{a^2}{3}+O(a^4),\\ 1-\frac{\langle B\rangle}{B_a}&=\frac{d^2}{12\lambda_L^2} +O(d^4/\lambda_L^4). \end{aligned}

Thus the parallel-field diamagnetic response is small even for a perfectly coherent thin slab.

Take Lg=10 pHL_g=10\,\mathrm{pH}, Lk=90 pHL_k=90\,\mathrm{pH}, Φext=0\Phi_{\rm ext}=0 and winding branch n=1n=1. Find II and Φ\Phi. Check them by minimizing the magnetic plus kinetic energy at fixed external flux.

Solution I=Φ0100 pH≃20.68 μA,Φ=LgI=0.1Φ0.\begin{aligned} I&=\frac{\Phi_0}{100\,\mathrm{pH}} \simeq20.68\,\mu\mathrm A,\\ \Phi&=L_gI=0.1\Phi_0. \end{aligned}

For general nn and external flux, the two inductive energies are

E(Φ)=(Φ−Φext)22Lg+(nΦ0−Φ)22Lk.E(\Phi)=\frac{(\Phi-\Phi_{\rm ext})^2}{2L_g} +\frac{(n\Phi_0-\Phi)^2}{2L_k}.

Setting its derivative to zero gives

Φ=LkΦext+LgnΦ0Lg+Lk.\Phi=\frac{L_k\Phi_{\rm ext}+L_gn\Phi_0}{L_g+L_k}.

At zero applied flux, n=0n=0 has lower energy; the stated n=1n=1 solution is a possible trapped branch, provided a phase-slip barrier and a sufficiently low current support it. Quantization constrains the fluxoid even though this branch contains only one tenth of a flux quantum of magnetic flux.

For Bz=B0e−qxB_z=B_0e^{-q x} and real σn>0\sigma_n>0, show that the surface power equals the integrated quasiparticle Joule heating. Use e−iωte^{-i\omega t}.

Solution

Write q=a−ibq=a-ib with a>0a>0. From q2=λL−2−iμ0ωσnq^2=\lambda_L^{-2}-i\mu_0\omega\sigma_n,

2ab=μ0ωσn.2ab=\mu_0\omega\sigma_n.

Also Ey(x)=ZsHz(0)e−qxE_y(x)=Z_s H_z(0)e^{-q x}. Therefore

PbulkA=σn2∫0∞∣Ey∣2dx=σn∣ZsHz(0)∣24a.\begin{aligned} \frac{P_{\rm bulk}}{A} &=\frac{\sigma_n}{2}\int_0^\infty|E_y|^2dx\\ &=\frac{\sigma_n|Z_sH_z(0)|^2}{4a}. \end{aligned}

Since Zs=−iμ0ω/qZ_s=-i\mu_0\omega/q, its real part is Rs=μ0ωb/(a2+b2)>0R_s=\mu_0\omega b/(a^2+b^2)>0. Substituting 2ab=μ0ωσn2ab=\mu_0\omega\sigma_n gives Pbulk/A=Rs∣Hz(0)∣2/2P_{\rm bulk}/A=R_s|H_z(0)|^2/2. Reversing the imaginary sign of λ~\widetilde\lambda without changing the time convention would incorrectly predict negative absorption.

A film has d=20 nmd=20\,\mathrm{nm} and λL=200 nm\lambda_L=200\,\mathrm{nm}. Estimate the mean parallel-field reduction and the Pearl scale. Why are these different questions?

Solution

The slab result gives 1−⟨B⟩/Ba≃0.12/12=8.33×10−41-\langle B\rangle/B_a\simeq0.1^2/12=8.33\times10^{-4}. For a perpendicular vortex or laterally varying field,

ΛP=2(200 nm)220 nm=4.0 μm.\Lambda_P=\frac{2(200\,\mathrm{nm})^2}{20\,\mathrm{nm}} =4.0\,\mu\mathrm m.

The first result concerns variation through the thickness; the second concerns currents and stray fields over lateral distances. Neither can replace the other by substituting a single sample dimension.

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