Skin Effect and Proximity Effect: How Litz Wire Solves the Loss Problem

The skin effect is the crowding of alternating current toward the surface of a conductor, which follows from Maxwell's equations: the current density decays exponentially into the depth, with a characteristic length δ = √(2/ωμσ), called the skin depth. The proximity effect is the additional eddy currents induced in a conductor by neighboring conductors carrying an alternating field; in a multilayer winding its contribution grows as the square of the number of layers. Litz wire suppresses both effects by dividing the copper cross-section into many insulated, transposed strands.

The problem of conductor losses under alternating current has an exact mathematical origin — Maxwell's equations. Not empirical lookup tables, not engineering intuition, but specific differential equations from which both the skin effect and the proximity effect are derived rigorously. In this article we work top-down: from the equations to the current density across the wire cross-section, to the Dowell equation for real windings, and to the modern numerical methods used today to compute losses in litz-wire coils.

Where the skin effect comes from: five lines from Maxwell

Inside a conductor carrying alternating current, three of Maxwell's four equations are at work — Faraday's law, Ampère's law without the displacement current (at frequencies up to hundreds of MHz it can be neglected in copper), and Ohm's law in local form:

Faraday's law
∇ × E = − ∂B∂t
a changing field induces an EMF
Ampère's law
∇ × H = J
(without displacement current)
Ohm's law
J = σE
local form
E
electric field strength, V/m
B
magnetic flux density, T (= V·s/m²)
H
magnetic field strength, A/m
J
electric current density, A/m²
σ
electrical conductivity of the material, S/m (for copper at 20 °C: σCu = 5.96·10⁷ S/m)
t
time, s

Substitute one into another, apply the curl identity, and for the sinusoidal regime at frequency ω we obtain the Helmholtz equation for the current density:

∇2J = jωμσ J
ω
angular frequency, rad/s (ω = 2πf, where f is the frequency in Hz)
μ
absolute magnetic permeability of the material, H/m (μ = μ₀·μr; for copper μr ≈ 1, so μ ≈ μ₀ = 4π·10⁻⁷ H/m)
j
imaginary unit

The solution for a semi-infinite conductor decays exponentially into the depth:

J(x) = J0 · e−x/δ · e−jx/δ
J(x)
current density at depth x from the surface, A/m²
J0
current density at the conductor surface, A/m²
x
coordinate into the depth of the conductor, m
δ
skin depth, m

And the skin depth itself is:

δ = √ 2ωμσ
δ
skin depth, m
ω
angular frequency, rad/s (ω = 2πf)
μ
absolute magnetic permeability, H/m (for copper ≈ μ₀ = 4π·10⁻⁷ H/m)
σ
conductivity, S/m (for copper at 20 °C: 5.96·10⁷ S/m)

The current falls off exponentially and at the same time lags in phase: at each depth δ the amplitude is attenuated by a factor of e ≈ 2.72, and the phase lags by 1 radian. At a depth of 5δ from the surface the current density is already less than 1% of the surface value.

Plot: the current density J(x)/J₀ falls exponentially into the depth of the conductor. At a depth of 1δ — 37%, 2δ — 14%, 3δ — 5%, 5δ — less than 1%.
Exponential decay of current density with depth: the solution of the Helmholtz equation e−x/δ. The shaded band is the engineering approximation "current flows in a layer of thickness δ," which discards another 37% of the current as nonexistent.

This is fundamental, and from it follows a non-obvious point: there is no "boundary" between a conducting region and a non-conducting one. Current is everywhere — it is simply negligibly small deep inside. The engineering approximation "current flows in a layer of thickness δ" is convenient but inaccurate.

The exact loss power accounts for the exponential tail and gives, per unit of surface area:

Pskin = 12σδ · |H0|2
Pskin
loss power per unit of surface area, W/m²
H0
amplitude of the tangential component of the magnetic field at the conductor surface, A/m
σ
conductivity, S/m
δ
skin depth, m

This formula is the basis for all the calculations that follow.

Round wire: the exact Bessel solution

The semi-infinite approximation works only for a flat conductor. For a round strand the problem is solved exactly through Bessel functions of the first kind with a complex argument. The current density as a function of radius r:

J(r) = J0 · J0(kr) J0(ka) k = 1 − j δ
J(r)
current density at radius r from the wire axis, A/m²
J0
(before the fraction) current density on the axis in the absence of the skin effect, A/m²
J0(·)
Bessel function of the first kind, order zero, dimensionless
r
radial coordinate inside the wire, m
a
outer radius of the wire, m
k
complex wave number in the conductor, 1/m

From this we obtain the exact ratio of AC to DC resistance:

FRskin = RACRDC = ka2 · Re [ J0(ka) J1(ka) ]
RAC
AC resistance at the given frequency, Ω
RDC
DC resistance, Ω
J1(·)
Bessel function of the first kind, order one
FRskin
dimensionless resistance-increase factor due to the skin effect alone (always ≥ 1)

In practice an approximation through the dimensionless parameter Q = d/δ — the ratio of strand diameter to skin depth — is used:

Q = d/δ FR (skin) What it means
0.51.0002skin effect imperceptible
1.01.005<1% increase
2.01.088% — the application limit for thin strands
3.01.3232% — the wire is "tired"
5.02.04already twice as bad as DC
103.8catastrophe

It is precisely from this table that the working criterion for choosing the strand in litz wire follows: Q ≤ 1, that is, d ≤ δ. Not "up to 2δ," as handbooks often state — that is the upper limiting boundary, while the practical optimum lies deeper.

Take a copper wire 1 mm in diameter at 1 MHz. The skin depth δ ≈ 66 µm, Q ≈ 15. The current density on the wire axis is roughly 0.01% of the surface value — the central part of the cross-section is electrically dead. The wire still "conducts," but only through a thin tube near the surface. Replace it with litz wire made of 100 strands of 0.1 mm (Q = 1.5, FR ≈ 1.03), and current flows again across the entire copper area.

Proximity effect: the Dowell equation and why layers kill

The skin effect is the wire's reaction to its own field. The proximity effect is the reaction to an external field created by its neighbors. And this is where the physics turns unkind.

In 1966 P. L. Dowell published "Effects of eddy currents in transformer windings" (Proc. IEE, vol. 113), in which he derived an analytical solution for a multilayer winding made of flat foil. The idea is simple: he replaced the round wires in a layer with an equivalent foil of the same copper area, solved the one-dimensional problem, and obtained a formula for the AC resistance of an m-layer winding:

FR = Δ · [ sinh 2Δ + sin 2Δ cosh 2Δ − cos 2Δ + 2(m2 − 1) 3 · sinh Δ − sin Δ cosh Δ + cos Δ ]
FR = RAC/RDC
total resistance-increase factor (skin + proximity), dimensionless
Δ
reduced conductor thickness, dimensionless: for a round wire Δ = (d/δ) · √(πη/4)
m
number of winding layers in the window, dimensionless
η
winding-layer fill factor (see below)

The model contains one important coefficient that Dowell introduced for the transition from foil to round wire — the winding-layer fill factor η (in the English-language literature, the porosity factor):

η = N · db
η
winding-layer fill factor, dimensionless (0 < η ≤ 1)
N
number of turns in one layer, count
d
wire diameter (copper), m
b
width of the winding layer in the core window, m

This is not the same as the window fill factor familiar from transformer design, kfill = Scopper/Swindow — the latter is two-dimensional (the copper fraction over the area of the whole window), whereas η is one-dimensional and describes the packing density of turns along a single coordinate (along the layer). And it has nothing to do with the geological "porosity coefficient" from building codes and standards, despite the similar English name — there it refers to the void volume in soil.

The physical meaning of η is simple: η → 1 for tight packing of turns butted together, η → 0 for a sparse winding with large gaps. In the Dowell formula η enters as a factor √η inside Δ, and for a loose winding the losses decrease — the magnetic field is "smeared" over a larger volume and links with less copper. This explains the old engineering trick with a spacer cord in high-Q resonant-circuit coils: an artificially sparse layout reduces the proximity effect.

Don't be intimidated by the hyperbolic-trigonometric expression itself. What matters is this: the second bracket contains the factor (m² − 1). Proximity-effect losses grow as the square of the number of winding layers. One layer — no proximity effect at all, only the skin effect works. Two layers — already three times more. Five layers — 24 times more than a single layer.

To see numbers rather than formulas, take a typical example from the Ridley Engineering handbook (2019): a transformer winding of 5 layers of 0.3 mm copper wire at 100 kHz. The Dowell calculation gives an average resistance increase of 11.6 times. For the innermost layer it is 27 times. Increase the diameter to 0.6 mm in an attempt to "add copper and cut the losses," and the average jumps to 51 times, while the inner layer reaches 123. More copper, eight times more losses. This is a counterintuitive but rigorous result of one-dimensional electrodynamics.

Heat map: 5 layers of 0.3 mm copper-wire winding at 100 kHz. The inner layer at the core has F_R = 27, the outer one about 1.5. The average value is F_R = 11.6.
Distribution of the resistance-increase factor FR across the winding layers: those nearest the core operate in a stronger magnetic field and heat up 10–20 times more than the outer ones. Adding copper by increasing the strand diameter does not help — it makes the picture worse.

Litz wire breaks this catastrophe at the root: by replacing one thick strand with a hundred thin transposed ones, it moves the winding into a regime where d ≪ δ, and the first term in the Dowell formula (the skin effect proper) becomes negligible, while the second (proximity, ∝ m²) remains but with a small Δ, because the strand is thin.

Internal and external proximity: why they must be separated

In the works of Ferreira (1994) and Sullivan–Zhang (COMPEL 2014), the proximity effect in litz wire is split into two components, and this split is fundamental for understanding the physics.

  • External proximity — the field created by neighboring winding turns acts on the strand from "outside the bundle." It is precisely this that produces the (m² − 1) factor in the Dowell formula. It is fought with transposition + a sparse winding + interleaving of the primary and secondary windings in a transformer.
  • Internal proximity — the field created by other strands within the same bundle acts on a given strand. It leads to that counterintuitive effect: naively splitting a thick wire into many thin strands can increase the losses if d has not dropped noticeably below δ. It is fought by choosing a sufficiently thin strand and the right packing.

Quantitatively: the integral Pprox in a litz-wire winding is the sum of two contributions — the external grows as m², the internal as n (the number of strands in the bundle). With proper design both terms are roughly equal — and that is the optimum. A strong imbalance in either direction means that there are either too few strands (the external contribution is overloaded) or too many (the internal is overloaded, and the enamel has eaten up the copper cross-section).

How the Q factor sees it: Q(f) and its peak

Everything said above concerns copper losses. But for an engineer designing a high-Q resonant circuit or a resonant converter, an integral parameter matters more: the coil Q factor Q = ωL/R. This is the very same letter Q as in the dimensionless parameter Q = d/δ, but it means something entirely different — the ratio of stored energy to energy lost per cycle. We will call it Qcoil to avoid confusion.

At low frequencies:

Qcoil ≈ 2πfLRDC
Qcoil
coil Q factor, dimensionless
f
frequency, Hz
L
coil inductance, H
RDC
DC resistance of the winding, Ω

Qcoil grows linearly with frequency — the inductive reactance rises while the resistive part stays at the DC level. But as we approach the region where Q = d/δ becomes of order one, the denominator begins to swell because of FR(f):

Qcoil(f) = 2πfL RDC · FR(f)
FR(f)
frequency-dependent resistance-increase factor (from Dowell or FEA), dimensionless, FR(f) ≥ 1

Because FR grows faster than linearly under Dowell, beyond a certain frequency Qcoil reaches a maximum and begins to decline. This maximum is the optimal operating point of the coil, and it is what engineers look for in design. For litz-wire coils in induction heaters the Qcoil peak typically falls at 30–100 kHz; for Qi wireless-charging coils, at 100–200 kHz; for MRI coils, at tens of MHz (using special constructions).

Elektrisola publishes direct measurements of Q(f) for its standard litz wires. A typical coil of 120 strands of 0.1 mm on an air core shows a maximum Qcoil ≈ 500 at 200 kHz — 2–3 times higher than a comparable coil of single-strand copper wire of the same DC-equivalent area. This is exactly the engineering gain for which litz wire is made.

Coil Q-factor plot Q(f) on a logarithmic scale. Litz wire 120×0.1 mm reaches a maximum Q ≈ 500 around 200 kHz and then declines; a single-strand 1 mm wire plateaus and drops sharply earlier.
Q factor Qcoil(f) = 2πfL/(RDC·FR(f)) for three constructions. The litz-wire working zone, 10 kHz to 1 MHz, is the highlighted band. The litz-wire peak is many times higher than that of single-strand wire of the same copper cross-section.

Three frequency bands — and where litz wire actually works

Modern models (Wojda & Kazimierczuk, 2012; Geng et al., IET Power Electronics, 2021) divide the operation of litz wire into three regimes:

Regime Q = d/δ What happens
Low frequencies Q ≪ 1 FR ≈ 1. DC resistance dominates; litz wire is excessive and merely adds mass because of the enamel insulation.
Mid frequencies Q ≈ 0.5–1.5 the optimum region. FR grows moderately, and litz wire cuts losses several-fold. This is 10 kHz to 1 MHz for diameters of 0.05–0.2 mm — induction heaters, Qi charging, PFC, LLC.
High frequencies Q ≫ 2 bundle-level proximity and inter-strand capacitance begin to dominate. FR rises again, and litz wire loses its advantage over hollow or film conductors.

The boundary between the mid and high bands is a separate, interesting piece of physics.

Why litz wire dies above 2 MHz: inter-strand capacitance

Every pair of adjacent strands in litz wire is a microcapacitor. Enamel 5–15 µm thick with a relative permittivity εr ≈ 3.5–4 (polyurethane, polyesterimide) forms a flat gap. The inter-strand capacitance per unit length for a typical 0.1 mm litz wire comes out on the order of 1–10 pF/m per pair of adjacent strands, and accounting for the many hundreds of pairs — tens of nanofarads per meter of total capacitance.

At frequency f the reactance of this capacitance is:

XC = 12πfC
XC
capacitive reactance, Ω
f
frequency, Hz
C
capacitance, F

At 100 kHz for 10 nF we get 160 Ω — a thousand times larger than the ohmic resistance of the strands, so the capacitance does not interfere. At 5 MHz for the same capacitance it is only 3.2 Ω, already comparable to the AC resistance. Instead of flowing through the enamel (which is formally an insulator), the current begins to "spill over" between strands through the capacitive coupling. The transposition loses its meaning, and electrically the litz wire turns into a single thick strand.

Two further troubles add to this:

  • The self-resonant frequency (SRF) of the coil. The winding's parasitic capacitance resonates with the inductance at the SRF, above which the component stops being an inductance and becomes a capacitance. For litz-wire coils the SRF is usually 2–10 MHz.
  • Capacitive switching losses:
    PC = C · V2 · f
    PC
    capacitive losses, W
    V
    voltage amplitude across the capacitance, V
    C
    parasitic capacitance of the winding, F
    f
    switching frequency, Hz
    At frequencies above 1 MHz and voltages of 400–800 V these losses can exceed the gain from the reduced ohmic resistance. Paradoxically, in some flyback converters switching from single-strand wire to litz wire worsens the overall efficiency precisely because of this.

Practical takeaway: the working range of litz wire is 10 kHz to 1 MHz. With reservations, up to 2–3 MHz. Above 5 MHz, you are already into special constructions with increased enamel thickness or flat film conductors.

What is used today: from Dowell to 3D FEA

The Dowell equation is a one-dimensional approximation. For most transformers its accuracy is sufficient, but the deviation from reality can reach 60% with an unfortunate winding geometry (Nan & Sullivan, IEEE Trans. Power Electronics, 2009). This pushed the industry toward numerical methods.

Today's toolkit looks like this:

  • The Ferreira method (1994): an exact Bessel solution for each strand, supplemented by superposition of the magnetic fields of its neighbors. More accurate than Dowell for sparse windings, less accurate for dense ones.
  • Sullivan–Zhang (COMPEL 2014): an analytical model that accounts for the twist pitch, directions, and multistage construction. Implemented in MATLAB and released as open source on the Thayer School (Dartmouth) website.
  • 2D FEA with discrete transposition (Roy, Sakly, IEEE 2014): the key idea is to solve a 2D FEA for parallel strands and then mathematically "shuffle" them in the impedance matrix according to a given twisting protocol. Accuracy within 10% for the RAC/RDC ratio.
  • 3D FEA with a litz model in Ansys Maxwell: the litz wire is modeled as a single cylinder with anisotropic conductivity. This makes it possible to compute coils with thousands of turns without drawing each strand.

In 2022 Lin et al. proposed an effective homogenization method for transient FEA that compresses the computation of a 10,000-strand winding to a few minutes of CPU time. By comparison, directly modeling each strand in the same problem would take several days.

What this gives the practicing engineer: modern litz wire is not selected "from a lookup table." For a specific product an FEA model is run with the real geometry of the window, core, and gap — and the optimum number and diameter of strands is found, minimizing the sum of copper and core losses. Dowell has remained in the engineering textbooks, but in serious developments of EV onboard chargers (OBCs), medical MRI coils, and wireless charging, numerical models are at work.

Check the Dowell formulas on your own case

The online litz-wire winding calculator implements the skin depth δ(f), F_R per Dowell, the Sullivan–Zhang optimum, and selection per TU DSGT.685660.019 — a calculation from 6 parameters right in the browser, no registration.

Sources

  1. P. L. Dowell. Effects of eddy currents in transformer windings. Proceedings of the IEE, vol. 113, no. 8, pp. 1387–1394, August 1966.
  2. J. A. Ferreira. Improved analytical modeling of conductive losses in magnetic components. IEEE Trans. Power Electronics, vol. 9, no. 1, 1994.
  3. Xi Nan, C. R. Sullivan. An Improved Calculation of Proximity-Effect Loss in High-Frequency Windings of Round Conductors. IEEE Trans. Power Electronics, 2009.
  4. C. R. Sullivan, R. Y. Zhang. Analytical Model for Effects of Twisting on Litz-Wire Losses. COMPEL 2014. Dartmouth, Thayer School of Engineering.
  5. R. P. Wojda, M. K. Kazimierczuk. Winding resistance and power loss for inductors with litz and solid-round wires. IEEE 2016.
  6. H. Geng et al. Modelling and optimization of winding resistance for litz wire inductors. IET Power Electronics, 2021.
  7. D. Lin et al. An Efficient Method for Litz-Wire AC Loss Computation in Transient Finite Element Analysis. IEEE Trans. Magnetics, vol. 58, no. 5, 2022.
  8. S. Zurek. Proximity effect. Encyclopedia Magnetica, e-magnetica.pl.
  9. R. Ridley. Proximity Loss. Ridley Engineering Design Notes.
  10. Elektrisola. HF-Litz Wire Technical Information. elektrisola.com.
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