Derivation of the diffusion equation
The radiative transport equation is [8]
 |
(4.1) |
where
is the radiance (W cm-2sr-1) at position
r in the direction of the unit vector
.
The differential solid
angle
has the unit vector
as an outward normal. The
phase function
represents the fraction of light scattered
from the direction
into the direction
.
The phase
function is normalized such that it is unity when integrated over all
directions.
The scattering medium is an infinite slab with finite thickness and
infinite breadth. The inward normal to the top of the slab is chosen as
the positive z-direction. The top surface is illuminated with a
monodirectional flux
 |
(4.2) |
where
is a unit vector in the direction of the
z-axis and
is a unit vector in the direction of the incident
flux and
is the cosine of the angle
makes with the z-axis.
The delta function
is discussed in Appendix C. Historically, the factor of
is included so that an isotropic diffuse source F0(r) will result in
a flux of
at a surface,
 |
(4.3) |
If the irradiance E0(r) represents collimated light, then
.
Notice that
includes contributions from a
cone containing all vectors having
,
and not just
one particular azimuthal angle. This simplifies the mathematics by
eliminating any azimuthal dependence of radiance in the slab. The radiance
is a function of only the position r and the angle
.
The phase function is modelled as a delta-Eddington phase function
 |
(4.4) |
where
is the cosine of the angle
between the incident and the scattered light. The first term accounts for
strong scattering in the forward direction and the second term approximates
a more diffuse type of scattering. The parameter f determines the
fraction of light scattered into the forward peak (the delta function) and
g' denotes the degree of asymmetry in the diffuse portion of the
scattering. The factor of
is included for normalization.
Substituting Equation (4.4) into (4.1) yields
![\begin{displaymath}
(\hat\mathbf{s}\cdot\nabla)L(\mathbf{r},\hat\mathbf{s}) = -\...
...{s}') [1+3g'(\hat\mathbf{s}\cdot\hat\mathbf{s}')] \,
d\omega'
\end{displaymath}](img211.gif) |
(4.5) |
where the reduced scattering coefficient is
and the
transport coefficient is
.
The transport
and
reduced scattering
coefficients are less than the corresponding
total attenuation
and scattering coefficients
respectively and represent effective total attenuation and
scattering. The scattering coefficient is reduced because light scattered
into the forward peak of Equation (4.4) is indistinguishable
from unscattered light. The fraction of light not scattered into
the forward peak is (1-f), and consequently, the scattering coefficient
is reduced by a factor of (1-f). Thus the reduced scattering
coefficient
represents the amount of light scattered out of the
collimated portion of the radiance and into the diffuse portion of the
radiance.
The radiance is divided into collimated and diffuse components
 |
(4.6) |
The collimated radiance includes both the light scattered into a
direction parallel to the incident beam and any unscattered light. Because
the collimated radiance includes light scattered forward, the beam is
attenuated not by the usual total attenuation coefficient
but by
the transport coefficient
The collimated light is attenuated at
a rate proportional to the transport coefficient.
 |
(4.7) |
The amount of collimated light entering the slab is given by Equation
(4.2), less the amount of light lost to specular reflection from
the surface
 |
(4.8) |
where rs is the specular reflection coefficient given by the usual
Fresnel reflection formula for specular reflection for an angle of
incidence
![\begin{displaymath}
r_s = {1\over 2}\left[
{\sin^2(\theta_0-\theta_t)\over\sin^2...
...n^2(\theta_0-\theta_t)\over\tan^2(\theta_0+\theta_t)}
\right]
\end{displaymath}](img221.gif) |
(4.9) |
The incident and transmitted angles
and
are
related by Snell's law
where
nair and
ntissue are the indices of
refraction of air and tissue. The solution of Equation (4.7)
subject to the initial condition of Equation (4.8) is
 |
(4.10) |
where
is the distance incident light travels in tissue to
reach a depth z in the slab. Substituting Equation (4.6) into
(4.5) and simplifying using Equations (4.7) and
(4.10) yields
where
has been rewritten in terms of the spherical
angles determining
and
If
and
then
 |
(4.12) |
The Eddington or diffusion approximation characterizes the diffuse radiance
as a sum of a diffuse radiant fluence
and a diffuse radiant flux per unit area
Fd(r) These are
defined as the first two moments of the radiance
 |
(4.13) |
The diffuse radiance can then be expressed as
 |
(4.14) |
The factors of
and
in Equation (4.14)
result from normalization. Equation (4.14) represents the
first two terms of the Taylor expansion for the diffuse radiance
,
where
represents the isotropic and
Fd(r) the anisotropic contribution to the diffuse radiance.
Recalling the solid angle integration identities (see Appendix C)
 |
(4.15) |
and substituting Equation (4.14) into (4.11)
and using (4.15) to simplify yields the following equation
for the diffuse radiance
Integration of Equation (4.17) over all directions and
using relations (4.15) results in the following equation for
the diffuse flux
 |
(4.17) |
Here the L. H. S. represents the net change in the diffuse radiant
flux. This equals the intensity lost through absorption of the diffuse
radiant fluence plus that gained through scattering of collimated light
into the diffuse portion of the radiance. Multiplying Equation
(4.17) by
and integrating over all angles yields an
energy flux equation for the diffuse radiance which states that the change
in the diffuse fluence equals the diffuse flux lost to absorption plus that
gained from collimated light.
 |
(4.18) |
where
is the reduced transport
coefficient. The reduced transport coefficient incorporates forward
scattered light from the second term of the delta-Eddington phase function
into the collimated beam in much the same way that such light for the first
term was incorporated into expressions for the reduced scattering
coefficient. Taking the divergence of Equation (4.18) and
solving for
yields
 |
(4.19) |
Equating Equation (4.17) and (4.19) leads
to a Helmholtz equation
 |
(4.20) |
which is the well-known diffusion equation. The R. H. S. of this
equation represents the collimated irradiation source.
|