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Appendix 2A: AC Resistance of a Round Wire When the Skin Depth δ Is Comparable to the Radius a of the Wire

Appendix 2A: AC Resistance of a Round Wire When the Skin Depth δ Is Comparable to the Radius a of the Wire

We have shown in Section 2.2 that the parameters α and β are given by δ−1 in a good conductor. The approximations made in arriving at this result assumed that the loss tangent T = σc/ωε is large. Another way of stating the approximation is to say that the displacement current density jωεE˜ is neglected in comparison with the conduction current density σcE˜. The propagation constant γ = jk may be obtained in this case by neglecting the first term on the RHS of (2.4)

(2A.1)
γ2=k2=jωμσ=2πfμσejπ/2.

The wave equation for the current density J˜=σcE˜ is given by

(2A.2)
2J˜jωμσcJ˜=0.

For the cylindrical one-dimensional problem under consideration in this section

(2A.3)
J˜=z^Jρ,

and from Equation 2A.2, we obtain

(2A.4)
d2Jdρ2+1ρdJdρjωμσcJ=0.

This function is the Bessel equation considered in Section 2.15 and since the currentdensity is finite at the origin, we reject the function Y0 and choose J0:

(2A.5)
J=AJ0Tρ,

where

(2A.6)
T=jωμσc=j1/22δ.

Since T is complex, J0(Tρ) is also complex and has a real part and an imaginary part. The following special functions called Ber(x) and Bei(x) are defined and tabulated in many mathematical tables:

(2A.7)
Berx=ReJ0j1/2x,
(2A.8)
Beix=ImJ0j1/2x.

In terms of the current density J˜a at the surface of the conductor, the current density in the wire may be written as

(2A.9)
J˜ρ=J˜aBer2ρ/δ+Bei2ρ/δBer2a/δ+Bei2a/δ,0<ρ<a.

Figure 2A.1 shows |J(ρ)/Ja| versus the radius for two values of a/δ. The solid lines show the results based on Equation 2A.9. The broken lines are shown for comparison and are obtained assuming a parallel plane formula

(2A.10)
J˜ρJ˜a=eaρ/δ,aδ,

which is a good approximation when a ≫ δ. As expected, the solid and the broken curves are close for a/δ = 7.55 and differ considerably for a/δ = 2.39.

image

FIGURE 2A.1
(a) Current distribution in a cylindrical wire for different frequencies. (b) Actual and approximate (parallel plate formula) distribution in cylindrical wire. (From Ramo, S., Whinnery, J.R., and Van Duzer, T., Fields and Waves in Communication Electronics. p. 297. 1967. Copyright Wiley-VCH Verlag GmbH&Co. KGaA. Reproduced with permission.)

The magnetic field H˜ may be obtained from Equation 1.40 and it has only the ϕ component

(2A.11)
H˜ϕ=1jωμdE˜zdρ

and

(2A.12)
E˜z=J˜σc=AσcJ0Tρ=J˜aσcJ0TρJ0Ta.

Hence,

(2A.13)
H˜ϕ=J˜aσcTjωμJ0TρJ0Ta=J˜aTJ0TρJ0Ta.

From Ampere’s law,

(2A.14)
2πaH˜ϕ|ρ=a=2πaJ˜aTJ0TaJ0Ta=I˜.

The internal impedance per unit length is

(2A.15)
Zi=E˜z|ρ=aI˜=J˜a/σcI˜=TJ0Ta2πaσcJ0Ta.

Equation 2A.15 may be expressed in terms of Ber and Bei functions defined by Equations 2A.7 and 2A.8, respectively, giving

(2A.16)
R=ReZi=Rs2πaBerqBerqBeiqBeiqBerq2+Beiq2Ω/m,
(2A.17)
ωLi=Rs2πaBerqBerq+BeiqBeiqBerq2+Beiq2Ω/m,

where

(2A.18)
q=2aδ

and

(2A.19)
Rs=1σcδ=πfμσc.

Figure 2A.1 shows the current distribution for different frequencies.

Figure 2A.2 shows R′/Rs and ωLi/Rs versus a/δ. As expected, they reach the horizontal line 1 as a/δ tends to infinity.

image

FIGURE 2A.2
(a) Solid wire skin effect quantities compared with d.c. values. (b) Solid wire skin effect quantities compared with values from high-frequency formulas. (From Ramo, S., Whinnery, J. R., and Van Duzer, T., Fields and Waves in Communication Electronics. p. 297. 1967. Copyright Wiley-VCH Verlag GmbH&Co. KGaA. Reproduced with permission [1].)

Reference

  1. 1.Ramo, S., Whinnery, J. R., and Van Duzer, T., Fields and Waves in Communication Electronics, Wiley, New York, 1967.
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