1 Accelerating charges emit electromagnetic waves. In materials at non-zero tem- perature, charges jitter back and forth within a material due to their thermal energy, emitting thermal radiation. How much charges jitter at a given temperature relates to the material’s intrinsic conductivity (or permittivity). This relationship is quan- tified in the fluctuation-dissipation theorem that relates the auto-correlation in local current densityjjj((((r, ω)to the permittivity and temperature distribution
hjα(rrr, ω)jβ(rrr000, ω)i = 0ω=()
π Θ(ω,T)δ(rrr−rrr000)δαβ, (B.1) whereΘ(ω,T)=~ω/[ex p(~ω/kbT)−1)]is the mean energy of a harmonic oscillator and is the material permittivity. To solve for the local currents, we use the Green function formalism for the electric and magnetic fields (assuming non magnetic materials)
E
EE(rrr, ω)=∫
V
d3r0iωµ0←→
GGGE(rrr,rrr000, ω)jjj(rrr000, ω) (B.2) HHH(rrr, ω)= ∫
V
d3r0←→ G
GGH(rrr,rrr000, ω)jjj(rrr000, ω). (B.3) In our case, we are interested in the heat transferred from one half-space, labeled by subscript 1, into another half-space, labeled with subscript 2, separated from the first by a vacuum gap of thicknessd. The vacuum gap is labeled with subscript 3, as shown in the diagram in Figure B.1.
We must solve for the fields in medium 2, caused by a source charge in medium 1. For a source charge atrrr000= (RRR000,−z0), the Green functions for the fields atrrr = (rrr,z > d) are [113]
←→
GGGE(rrr,rrr000, ω)= i 4π2
∫ ∞
0
d2k||
1
kz1(stˆ21s sˆ+pˆ+2t21p pˆ+1)eikkk| |·(RRR−RRR000)eikz2(z−d)e−ikz1z0 (B.4)
1The derivation in this section follows closely that laid out in Joulain et al. [113] with some of the steps filled in. Other helpful resources are [145–147].
Figure B.1: Diagram of two layered half-spaces
←→
GGG H(rrr,rrr000, ω)= −n2ω 4π2c
∫ ∞
0
d2k||
1 kz1
(−pˆ+2t21s sˆ+stˆ21p pˆ+1)eikkk| |·(RRR−RRR000)eikz2(z−d)e−ikz1z0. (B.5) The wave vector components arekkk =(kkk||,kzzˆ), wherekkk|| is the in-plane wave vector andkz is the z-component, such thatk =q
(ωc)2−k2||. The unit vectors in Eqs.B.2 and B.3 are ˆs = kˆ|| × zˆ and ˆp±i = (k||zˆ∓ kzikˆ||)/(niω/c), and the term t21s,p is the generalized Fresnel coefficient from medium 2 into medium 1, where for a given polarizationsorp[146]
t12= t13t23eikz3d
1−r31r32e2ikz3d. (B.6) Ultimately, we are interested in the energy density that these fields convey from one medium to the other, or rather the mean z-component of the Poynting vector
hSzi= 1
2<hEEE ×HHH∗ ·zˆi = 1
2<hExHy∗−EyHx∗i. (B.7) Making use of Einstein’s summation convention, we find that the vector components of the above fields are in the following form:
Ai(rrr, ω)=C
∫ d3r0
∫
d2k||eikkk| |·(RRR−RRR000)eikz2(z−d)e−ikz1z0Gi jjj(rrr000)∀i, j ∈ {x,y,z}. (B.8) Hence, the terms in Eq. B.7 evaluate to
hExHy∗i=n∗2µ0ω2 16π4c
∫ d3r0
∫ d3r00
∫ d2k||
∫
d2k0|| 1
|kz1|2 eikkk| |·(RRR−RRR000)eikz2(z−d)e−ikz1z0e−ikkk0| |·(RRR−RR00
R0000)
e−ikz20∗(z−d)eikz10∗z00 (stˆ21s sˆ+pˆ+2t21p pˆ+1)x k(−pˆ+2t21s sˆ+stˆ21p pˆ+1)∗ylhjk(rrr000, ω)jl∗(rrr000000, ω)i.
(B.9)
Plugging in the fluctuation-dissipation theorem in Eq. B.1, we get hExHy∗i=n∗2µ0ω2
16π4c
∫ d3r0
∫ d3r00
∫ d2k||
∫
d2k0|| 1
|kz1|2 eikkk| |·(RRR−RRR000)eikz2(z−d)e−ikz1z0e−ikkk
0
| |·(RRR−RRR000000)
e−ikz20∗(z−d)eikz10∗z00 (stˆ21s sˆ+pˆ+2t21p pˆ+1)x k(−pˆ+2t21s sˆ+stˆ21p pˆ+1)∗yl0ω=(1)
π Θ(ω,T)δ(rrr000−rrr000000)δkl. (B.10) After applying the Kroenecker delta, and integrating overd3r00, we get
hExHy∗i=n∗2µ00ω3Θ(ω,T) 16π5c
∫ d3r0
∫ d2k||
∫
d2k0|| 1
|kz1|2=(1) eikkk| |·(RRR−RRR000)eikz2(z−d)e−ikz1z0e−ikkk
0
| |·(RRR−RRR000)
e−ikz20∗(z−d)eikz10∗z0 (stˆ21s sˆ+ pˆ+2t21p pˆ+1)x k(−pˆ+2t21s sˆ+stˆ21p pˆ+1)∗yk.
(B.11)
By the definition of r0, the differential d3r0 = d2R0dz0. Including this fact and further consolidating terms, we get
hExHy∗i=n∗2ω3Θ(ω,T) 16π5c3
∫ d2k||
∫
d2k0|| 1
|kz1|2=(1)eiRRR·(kkk| |−kkk
0
| |)
ei(kz2−kz20∗)(z−d) (stˆ21s sˆ+pˆ+2t21p pˆ+1)x k(−pˆ+2t21s sˆ+stˆ21p pˆ+1)∗
yk
∫ 0
−∞
dz0e(ikz10∗−ikz1)z0
∫
d2R0e−iRR0
R00·(kkk| |−kkk0
| |).
(B.12) The last integral equals 4π2δ(kkk|| −kkk0||). As kz is a function of k||, evaluating the integral overd2k0|| reducesk0z → kz, and we get
hExHy∗i=n∗2ω3Θ(ω,T) 4π3c3
∫ d2k||
1
|kz1|2=(1)e−2=(kz2)(z−d) (stˆ21s sˆ+pˆ+2t21p pˆ+1)x k(−pˆ+2t21s sˆ+stˆ21p pˆ+1)∗yk
∫ 0
−∞
dz0e2=(kz1)z0.
(B.13)
The last integral simplifies to 2=(k1
z1) such that hExH∗yi =n∗2ω3Θ(ω,T)
4π3c3
∫ d2k||
1
|kz1|2
=(1)
2=(kz1)e−2=(kz2)(z−d) (stˆ21s sˆ+pˆ+2t21p pˆ+1)x k(−pˆ+2t21s sˆ+stˆ21p pˆ+1)∗yk.
(B.14)
By symmetry of the indices the other half of the Poynting vector is hEyH∗xi=n∗2ω3Θ(ω,T)
4π3c3
∫ d2k||
1
|kz1|2
=(1)
2=(kz1)e−2=(kz2)(z−d) (stˆ21s sˆ+ pˆ+2t21p pˆ+1)yk(−pˆ+2t21s sˆ+stˆ21p pˆ+1)∗x k.
(B.15) All that remains is to sum over the Cartesian components k. Here, it is beneficial to assume without loss of generality that the in-plane wave vector is parallel to the x-axis, such that ˆk|| = x. By the definitions of ˆˆ s = kˆ|| × zˆ and ˆp±i = (k||zˆ∓ kzikˆ||)/(niω/c), we get the following dot product relations:
ˆ
s· xˆ= sˆ·zˆ =0, sˆ· yˆ = −1 pˆi±· xˆ= ∓kzi
niω/c, pˆ±i ·yˆ =0, pˆ±i ·zˆ= k||
niω/c. (B.16) It is also beneficial to adopt a more concise notation, where
gαβE =(stˆ21s sˆ+ pˆ+2t21p pˆ+1)αβ
gαβH∗ =(−pˆ+2t21s sˆ+stˆ21p pˆ+1)∗αβ. (B.17) Fork = x:
gEx xgH∗yx =
0+ −kz2
n2ω/ct21p −kz1
n1ω/c 0−1t21p∗
−k∗z1 n∗1ω/c
= kz2|kz1|2|t21p |2 n2|n1|2ω3/c3.
(B.18)
Fork = y:
gxEygy yH∗ =0. (B.19)
Fork = z:
gxzEgHyz∗ =
0+ −kz2
n2ω/ct21p k||
n1ω/c 0−1t21p∗ k||
n∗1ω/c
= kz2k2|||t21p |2 n2|n1|2ω3/c3.
(B.20)
Summing these three components together results in gx kE gH∗yk = kz2|t21p |2
n2|n1|2ω/c
k2||+|kz1|2 ω2/c2
!
. (B.21)
To evaluate the expression forhEyHx∗i, we must do the same calculation forgEykgHx k∗. Fork = x andk = z, this expression is 0. For k = y, we get
gEy ygxyH∗ = t21s +0 k∗z2
n∗2ω/ct21s∗(−1)+0
=−k∗z2|t21s |2 n∗2ω/c .
(B.22)
Hence the z-component of the Poynting vector, evaluated at the interface of the second half-spacez =d, is
hSz1→2i=<
1
2hExHy∗−EyHx∗i
=<
"
n∗2ω3Θ(ω,T1) 8π3c3
∫ d2k||
1
|kz1|2
=(1) 2=(kz1) kz2|t21p |2
n2|n1|2ω/c
k||2+|kz1|2 ω2/c2
!
+ k∗z2|t21s |2 n∗2ω/c
! # . (B.23) To simplify this expression, we use a number of useful identities: [113, 147]
=(i)ω2
c2 = 2<(kzi)=(kzi)
<(i∗kzi) = <(kzi)
|kzi|2+k2||
ω2/c2
=(i∗kzi) = =(kzi)
−|kzi|2+k2||
ω2/c2
(B.24) and we get
hSz1→2i = Θ(ω,T1) 8π3
∫ d2k||
1
|kz1|2 |t21s |2<(kz1)<(kz2) + |t21p |2<(1∗kz1)<(2∗kz2)
|n1|2n2|2
! .
(B.25)
After plugging in the expression for the generalized Fresnel coefficients from Eq. B.6 hSz1→2i= Θ(ω,T1)
8π3
∫ d2k||
1
|kz1|2
|t13s |2|t23s |2<(kz1)<(kz2)
|1−r13s r13s e2ikz0d|2 + |t13p |2|t23p |2<(1∗kz1)<(2∗kz2)
|n1|2n2|2|1−r13s r13s e2ikz0d|2
! .
(B.26)
For non-magnetic materials, the following identities hold:
<(kz3)(1− |r13|2) = <(kz1)|t13|2
<(kz3)(1− |r23|2) = <(kz2)|t23|2|kz3|2
|kz2|2
<(3∗kz3)(1− |r31p |2)+2=(3∗kz3)=(r13p) = <(1∗kz1)|t31p |2|n3|2
|n1|2
<(3∗kz3)(1− |r31p |2)+2=(3∗kz3)=(r23p) = <(2∗kz2)|t32p |2|n3|2
|n1|2
|3|2
|2|2
|kz3|2
|kz2|2,
wherer13,r23,t13, andt23are the Fresnel reflection and transmission coefficients of half-space 1 into vacuum and half-space 2 into vacuum, respectively. In medium 3, inside the vacuum gap, n3 = 3 = 1. Moreover, for propagating modes where k|| < ω/c, the z-component of the wave vector in vacuum is purely real,<(kz3) = kz3, =(kz3) = 0. On the other hand, for evanescent modes where k|| > ω/c, the opposite is true, <(kz3) = 0, =(kz3) = |kz3| . These facts allows us divide the integral in Eq. B.26 into a propagating part and an evanescent part. By applying in the identities in Eq. B.27 and the fact that for uniaxial mediad2k|| = 2πk||dk|| we get
hSz1→2i= Θ(ω,T1) 4π2
Õ
s,p
∫
k||dk||
(1− |r31s,p|2)(1− |r32s,p|2)
|1−r13s r13s e2ikz0d|2
+ 4=(r31s,p)=(r32s,p)
|1−r13s r13s e2ikz0d|2
! .
(B.27)
This expression is the power emitted from half-space 1 and absorbed by half-space 2. To get the net heat flux, we must also subtract the power emitted from half-space 2 back into half-space 1. The expression is identical to Eq. B.27, except the indices are reversed:
hSz2→1i= Θ(ω,T2) 4π2
Õ
s,p
∫
k||dk||
(1− |r31s,p|2)(1− |r32s,p|2)
|1−r13s r13s e2ikz0d|2
+ 4=(r31s,p)=(r32s,p)
|1−r13s r13s e2ikz0d|2
! .
(B.28)
As the expression inside the integral in Eqs. B.27 and B.28 is symmetric for indices 1 and 2, all that changes is the Bose-factor Θ. We define the spectral heat flux H(ω,T1,T2)as
H(ω,T1,T2)=Φ(ω) (Θ(ω,T1) −Θ(ω,T2)), (B.29) whereΦ(ω)is the transmissivity function, partitioned over propagating modes where k|| < ω/c, and evanescent modes wherek|| > ω/c[89],
Φ(ω)=Õ
s,p
∫ ω/c
0
dk||
k||
2π
(1− |r13s,p|2)(1− |r23s,p|2)
|1−r13s,pr23s,pei2kz0d|2 +
∫ ∞ ω/cdk||
k||
2π
4=(r13s,p)=(r23s,p)
|1−r13s,pr23s,pe−2|kz0|d|2.
(B.30)
This expression is also valid for layered media, where the Fresnel coefficients can be calculated by the transfer matrix method, as outlined in Appendix A [89]. To get
the total heat flux we integrate the Poynting vector over all frequencies such that Q(T1,T2)=
∫ ∞
0
dω
2πH(ω,T1,T2). (B.31)