Online: http://dust.ess.uci.edu/facts Updated: Sun 25th Jun, 2006, 11:59
Radiative Transfer in the Earth System
by Charlie Zender
University of California at Irvine

Department of Earth System Science zender@uci.edu
University of California Voice: (949) 824-2987
Irvine, CA  92697-3100 Fax: (949) 824-3256

Copyright © 2000–2005, Charles S. Zender
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Particle Size Distributions: Theory and Application to Aerosols, Clouds, and Soils
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Natural Aerosols in the Climate System
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Notes for Students of ESS 200B,
Earth System Physics:

This monograph on Radiative Transfer provides some core and some supplementary reading material for ESS 200B. We will discuss much of the material in the first twenty pages, and the figures at the end. The Index beginning on page 361 is also helpful.

Notes for Students of ESS 236,
Radiative Transfer and Remote Sensing:

Yada yada yada.

Contents

List of Figures
List of Tables
1 Introduction
 1.1 Planetary Radiative Equilibrium
 1.2 Fundamentals
2 Radiative Transfer Equation
 2.1 Definitions
  2.1.1 Intensity
  2.1.2 Mean Intensity
  2.1.3 Irradiance
  2.1.4 Actinic Flux
  2.1.5 Actinic Flux Enhancement
  2.1.6 Energy Density
  2.1.7 Spectral vs. Broadband
  2.1.8 Thermodynamic Equilibria
  2.1.9 Planck Function
  2.1.10 Hemispheric Quantities
  2.1.11 Stefan-Boltzmann Law
  2.1.12 Luminosity
  2.1.13 Extinction and Emission
  2.1.14 Optical Depth
  2.1.15 Geometric Derivation of Optical Depth
  2.1.16 Stratified Atmosphere
 2.2 Integral Equations
  2.2.1 Formal Solutions
  2.2.2 Thermal Radiation In A Stratified Atmosphere
  2.2.3 Angular Integration
  2.2.4 Thermal Irradiance
  2.2.5 Grey Atmosphere
  2.2.6 Scattering
  2.2.7 Phase Function
  2.2.8 Legendre Basis Functions
  2.2.9 Direct and Diffuse Components
  2.2.10 Source Function
  2.2.11 Radiative Transfer Equation in Slab Geometry
  2.2.12 Azimuthal Mean Radiation Field
  2.2.13 Anisotropic Scattering
  2.2.14 Diffusivity Approximation
  2.2.15 Transmittance
 2.3 Reflection, Transmission, Absorption
  2.3.1 BRDF
  2.3.2 Lambertian Surfaces
  2.3.3 Albedo
  2.3.4 Flux Transmission
 2.4 Two-Stream Approximation
  2.4.1 Two-Stream Equations
  2.4.2 Layer Optical Properties
  2.4.3 Conservative Scattering Limit
 2.5 Solar Heating
 2.6 Chapter Exercises
3 Remote Sensing
 3.1 Rayleigh Limit
 3.2 Anomalous Diffraction Theory
 3.3 Geometric Optics Approximation
 3.4 Single Scattered Intensity
 3.5 Satellite Orbits
 3.6 Aerosol Characterization
  3.6.1 Measuring Aerosol Optical Depth
  3.6.2 Aerosol Indirect Effects on Climate
  3.6.3 Aerosol Effects on Snow and Ice Albedo
  3.6.4 Ångstrøm Exponent
4 Gaseous Absorption
 4.1 Line Shape
  4.1.1 Line Shape Factor
  4.1.2 Natural Line Shape
  4.1.3 Pressure Broadening
  4.1.4 Doppler Broadening
  4.1.5 Voigt Line Shape
5 Molecular Absorption
 5.1 Mechanical Analogues
  5.1.1 Vibrational Transitions
  5.1.2 Isotopic Lines
  5.1.3 Combination Bands
 5.2 Partition Functions
 5.3 Dipole Radiation
 5.4 Two Level Atom
 5.5 Line Strengths
  5.5.1 hitran
 5.6 Line-By-Line Models
  5.6.1 Literature
6 Band Models
 6.1 Generic
  6.1.1 Beam Transmittance
  6.1.2 Beam Absorptance
  6.1.3 Equivalent Width
  6.1.4 Mean Absorptance
 6.2 Line Distributions
  6.2.1 Line Strength Distributions
  6.2.2 Normalization
  6.2.3 Mean Line Intensity
  6.2.4 Mean Absorptance of Line Distribution
  6.2.5 Transmittance
  6.2.6 Multiplication Property
 6.3 Transmission in Inhomogeneous Atmospheres
  6.3.1 Constant mixing ratio
  6.3.2 H-C-G Approximation
 6.4 Temperature Dependence
 6.5 Transmission in Spherical Atmospheres
  6.5.1 Chapman Function
7 Radiative Effects of Aerosols and Clouds
 7.1 Single Scattering Properties
  7.1.1 Maxwell Equations
 7.2 Separation of Variables
  7.2.1 Azimuthal Solutions
  7.2.2 Polar Solutions
  7.2.3 Radial Solutions
  7.2.4 Plane Wave Expansion
  7.2.5 Boundary Conditions
  7.2.6 Mie Theory
  7.2.7 Resonances
  7.2.8 Optical Efficiencies
  7.2.9 Optical Cross Sections
  7.2.10 Optical Depths
  7.2.11 Single Scattering Albedo
  7.2.12 Asymmetry Parameter
  7.2.13 Mass Absorption Coefficient
 7.3 Effective Single Scattering Properties
  7.3.1 Effective Efficiencies
  7.3.2 Effective Cross Sections
  7.3.3 Effective Specific Extinction Coefficients
  7.3.4 Effective Optical Depths
  7.3.5 Effective Single Scattering Albedo
  7.3.6 Effective Asymmetry Parameter
 7.4 Mean Effective Single Scattering Properties
  7.4.1 Mean Effective Efficiencies
  7.4.2 Mean Effective Cross Sections
  7.4.3 Mean Effective Specific Extinction Coefficients
  7.4.4 Mean Effective Optical Depths
  7.4.5 Mean Effective Single Scattering Albedo
  7.4.6 Mean Effective Asymmetry Parameter
 7.5 Bulk Layer Single Scattering Properties
  7.5.1 Addition of Optical Properties
  7.5.2 Bulk Optical Depths
  7.5.3 Bulk Single Scattering Albedo
  7.5.4 Bulk Asymmetry Parameter
  7.5.5 Diagnostics
8 Global Radiative Forcing
9 Implementation in NCAR models
10 Appendix
 10.1 Vector Identities
 10.2 Legendre Polynomials
 10.3 Spherical Harmonics
 10.4 Bessel Functions
  10.4.1 Spherical Bessel Functions
  10.4.2 Recurrence Relations
  10.4.3 Power Series Representation
  10.4.4 Asymptotic Values
 10.5 Gaussian Quadrature
 10.6 Exponential Integrals
Bibliography
Index

List of Figures

Cross Section and Quantum Yield of Nitrogen Dioxide
Vertical Distribution of Photodissociation Rates
Climatological Mean Absorbed Solar Radiation
Climatological Mean Emitted Longwave Radiation
ENSO Temperature and OLR
Seasonal Shortwave Cloud Forcing
Zonal Mean Shortwave Cloud Forcing
Seasonal Longwave Cloud Forcing
Zonal Mean Longwave Cloud Forcing
10 Climatological Mean Net Cloud Forcing
11 ENSO Cloud Forcing

List of Tables

facts
Wave Parameter Conversion Table
Actinic Flux Enhancement
Surface Albedo
Temperature Dependence of αp
Pressure-Broadened Half Widths
Mechanical Analogues of Important Gases
hitran database
Full-range Gaussian quadrature
10 Half-range Gaussian quadrature

1 Introduction

This document describes mathematical and computational considerations pertaining to radiative transfer processes and radiative transfer models of the Earth system. Our approach is to present a detailed derivation of the tools of radiative transfer needed to predict the radiative quantities (irradiance, mean intensity, and heating rates) which drive climate. In so doing we begin with discussion of the intensity field which is the quantity most often measured by satellite remote sensing instruments. Our approach owes much to Bohren and Huffman [1983] (particle scattering), Goody and Yung [1989] (band models), and Thomas and Stamnes [1999] (nomenclature, discrete ordinate methods, general approach). The nomenclature follows these authors where possible. These sections will evolve and differentiate from their original sources as the manuscript takes on the flavor of the researchers who contribute to it.

1.1 Planetary Radiative Equilibrium

The important role that radiation plays in the climate system is perhaps best illustrated by a simple example showing that without atmospheric radiative feedbacks (especially, ironically, the greenhouse effect), our planet’s mean temperature would be well below the freezing point of water. Earth is surrounded by the near vacuum of space so the only way to transport energy to or from the planet is via radiative processes. If E is the thermal energy of the planet, and FASR and FOLR are the absorbed solar radiation and emitted longwave radiation, respectively, then

∂E        ASR     OLR
---- =  F     - F                                    (1 )
∂t
On timescales longer than about a year the Earth as a whole is thought to be in planetary radiative equilibrium. That, is, the global annual mean planetary temperature is nearly constant because the absorbed solar energy is exactly compensated by thermal radiation lost to space over the course of a year. Thus
FASR   =  F OLR                                   (2 )
The total amount of solar energy available for the Earth to absorb is the incoming solar flux (or irradiance) at the top of Earth’s atmosphere, F (aka the solar constant), times the intercepting area of Earth’s disk which is πr2. Since Earth rotates, the total mean incident flux πr 2F is actually distributed over the entire surface area of the Earth. The surface area of a sphere is four times its cross-sectional area so the mean incident flux per unit surface area is F4. The fraction of incident solar flux which is reflected back to space, and thus unable to heat the planet, is called the aplanetary albedo or spherical albedo, . Satellite observations show that ℛ≈ 0.3. Thus only (1 -ℛ) of the mean incident solar flux contributes to warming the planet and we have
  ASR
F      =   (1 - ℛ)F  ⊙∕4                               (3 )

Earth does not cool to space as a perfect blackbody (41a) of a single temperature and emissivity. Nevertheless the spectrum of thermal radiation FOLR which escapes to space and thus cools Earth does resemble blackbody emission with a characteristic temperature. The effective temperature TE of an object is the temperature of the blackbody which would produce the same irradiance. Inverting the Stefan-Boltzmann Law (73) yields

TE   ≡   (FOLR ∕σ)1∕4                                (4 )
For a perfect blackbody, T = TE. For a planet, the difference between TE and the mean surface temperature Ts is due to the radiative effects of the overlying atmosphere. The insulating behavior of the atmosphere is more commonly known as the greenhouse effect.

Substituting (3) and (4) into (2)

(1 - ℛ)F  ∕4  =   σT 4                                      (5 )
         ⊙        (  E         )
                    (1 --ℛ)F-⊙- 1∕4
          TE  =         4σ                                  (6 )
For Earth, ℛ≈ 0.3 and F 1367 W m-2. Using these values in (6) yields T E = 255 K. Observations show the mean surface temperature Ts = 288 K.

1.2 Fundamentals

The fundamental quantity describing the electromagnetic spectrum is frequency, ν. Frequency measures the oscillatory speed of a system, counting the number of oscillations (waves) per unit time. Usually ν is expressed in cycles-per-second, or Hertz. Units of Hertz may be abbreviated Hz, hz, cps, or, as we prefer, s-1. Frequency is intrinsic to the oscillator and does not depend on the medium in which the waves are travelling. The energy carried by a photon is proportional to its frequency

E  =   hν                                      (7 )
where h is Planck’s constant. Regrettably, almost no radiative transfer literature expresses quantities in frequency.

A related quantity, the angular frequency ω measures the rate of change of wave phase in radians per second. Wave phase proceeds through 2π radians in a complete cycle. Thus the frequency and angular frequency are simply related

ω   =  2π ν                                     (8 )
Since radians are considered dimensionless, the units of ω are s-1. However, angular frequency is also rarely used in radiative transfer. Thus some authors use the symbol ω to denote the element of solid angle, as in dω. The reader should be careful not to misconstrue the two meanings. In this text we use ω only infrequently.

Most radiative transfer literature use wavelength or wavenumber. Wavelength, λ (m), measures the distance between two adjacent peaks or troughs in the wavefield. The universal relation between wavelength and frequency is

λν  =   c                                      (9 )
where c is the speed of light. Since c depends on the medium, λ also depends on the medium.

The wavenumber ~ν m-1, is exactly the inverse of wavelength

~ν  ≡   1-=  ν-                                 (10 )
       λ    c
Thus ν~ measures the number of oscillations per unit distance, i.e., the number of wavecrests per meter. Using (9) in (10) we find ~ν = ν∕c so wavenumber ~ν is indeed proportional to frequency (and thus to energy). Historically spectroscopists have favored ~ν rather than λ or ν. Because of this history, it is much more common in the literature to find ~ν expressed in CGS units of cm-1 than in SI units of m-1. The CGS wavenumber is used analogously to frequency and to wavelength, i.e., to identify spectral regions. The energy of radiative transitions are commonly expressed in CGS wavenumber units. The relation between ν~ expressed in CGS wavenumber units (cm-1) and energy in SI units (J) is obtained by using (10) in (7)
E   =   100hcν                                  (11 )

There is another, distinct quantity also called wavenumber. This secondary usage of wavenumber in this text is the traditional measure of spatial wave propagation and is denoted by k.

k  ≡   2π~ν                                   (12 )
The wavenumber k is set in Roman typeface as an additional distinction between it and other symbols 1.

Table 2 summarizes the relationships between the fundamental parameters which describe wave-like phenomena.



Table 2: Wave Parameter Conversion Tablea b







Variable ν λ                        ~ν ω k τ
Units s-1 m cm-1 s-1 m-1 s







ν -              c-
             ν                       -ν---
                      100c 2πν                                            2π-ν
                                             c                                                        1-
                                                       ν
       
λ    c-
   λ -                       -1---
                      100λ                                  2πc-
                                  λ                                             2π-
                                            λ                                                        λ-
                                                       c
       
~ν 100c     ν~            --1--
           100~ν -                                 --~ν---
                                200πc 200π                                               ~ν                                                      --1---
                                                     100c~ν
       
ω    ω--
   2π             2πc-
             ω                      --ω---
                     200πc -                                             ω-
                                             c                                                       2π-
                                                       ω
       
k    kc
   2π-              2π
             k--                        k
                      200π- ck -                                                       2π
                                                      ck-
       
τ    1
   --
   τ                        1
                     ------
                     100cτ                                  2π
                                 ---
                                  τ                                             2π
                                            ---
                                            cτ -







       

2 Radiative Transfer Equation

2.1 Definitions

2.1.1 Intensity

The fundamental quantity defining the radiation field is the specific intensity of radiation. Specific intensity, also known as radiance, measures the flux of radiant energy transported in a given direction per unit cross sectional area orthogonal to the beam per unit time per unit solid angle per unit frequency (or wavelength, or wavenumber). The units of Iλ are Joule meter-2 second-1 steradian-1 meter-1. In SI dimensional notation, the units condense to J m-2 s-1 sr-1 m-1. The SI unit of power (1 Watt 1 Joule per second) is preferred, leading to units of W m-2 sr-1 m-1. Often the specific intensity is expressed in terms of spectral frequency Iν with units W m-2 sr-1 Hz-1 or spectral wavenumber (also I~ν) with units W m-2 sr-1 (cm-1)-1.

Consider light travelling in the direction ˆΩ through the point r. Construct an infinitesimal element of surface area dS intersecting r and orthogonal to ˆΩ. The radiant energy dE crossing dS in time dt in the solid angle in the frequency range [ν,ν + dν] is related to Iν(r, ˆ
Ω) by

dE  = Iν(r, ˆΩ, t,ν) dS dt dΩ dν
(13)

It is not convenient to measure the radiant flux across surface orthogonal to Ωˆ, as in (13), when we consider properties of radiation fields with preferred directions. If instead, we measure the intensity orthogonal to an arbitrarily oriented surface element dA with surface normal ˆn, then we must alter (13) to account for projection of dS onto dA. If the angle between ˆn and ˆΩ is θ then

cos θ = ˆn ⋅ ˆΩ
(14)

and the projection of dS onto dA yields

dA =  cosθ dS
(15)

so that

dE  = Iν(r,Ωˆ, t,ν)cos θdA  dtdΩ d ν
(16)

The conceptual advantage that (16) has over (13) is that (16) builds in the geometric factor required to convert to any preferred coordinate system defined by dA and its normal ˆn. In practice dA is often chosen to be the local horizon.

The radiation field is a seven-dimensional quantity, depending upon three coordinates in space, one in time, two in angle, and one in frequency. We shall usually indicate the dependence of spectral radiance and irradiance on frequency by using ν as a subscript, as in Iν, in favor of the more explicit, but lengthier, notation I(ν). Three of the dimensions are superfluous to climate models and will be discarded: The time dependence of Iν is a function of the atmospheric state and solar zenith angle and will only be discussed further in those terms, so we shall drop the explicitly dependence on t. We reduce the number of spatial dimensions from three to one by assuming a stratified atmosphere which is horizontally homogeneous and in which physical quantities may vary only in the vertical dimension z. Thus we replace r by z. This approximation is also known as a plane-parallel atmosphere, and comes with at least two important caveats: The first is the neglect of horizontal photon transport which can be important in inhomogeneous cloud and surface environments. The second is the neglect of path length effects at large solar zenith angles which can dramatically affect the mean intensity of the radiation field, and thus the atmospheric photochemistry.

With these assumptions, the intensity is a function only of vertical position and of direction, Iν(z,ˆΩ). Often the optical depth τ (defined below), which increases monotonically with z, is used for the vertical coordinate instead of z. The angular direction of the radiation is specified in terms of the polar angle θ and the azithumal angle φ. The polar angle θ is the angle between ˆ
Ω and the normal surface nˆ that defines the coordinate system. The specific intensity of radiation traveling at polar angle θ and azimuthal angle φ at optical depth level τ in a plane parallel atmosphere is denoted by Iν(τ,θ,φ). Specific intensity is also referred to as intensity.

Further simplification of the intensity field is possible if it meets certain criteria. If Iν is not a function of position (τ), then the field is homogeneous. If Iν is not a function of direction (ˆ
Ω), then the field is isotropic.

2.1.2 Mean Intensity

The mean intensity is an integrated measure of the radiation field at any point r. Mean intensity ˉI ν is defined as the mean value of the intensity field integrated over all angles.

     ∫
     -Ω-Iν d-Ω
ˉIν =  ∫  dΩ                                      (17 )
       Ω
The solid angle subtended by Ω is the ratio of the area A enclosed by Ω on a spherical surface to the square of the radius of the sphere. Since the area of a sphere is 4πr2, there must be 4π steradians in a sphere. It is straightforward to demonstrate that the differential element of area in spherical polar coordinates is r2 sin θ dθ dφ. Thus the element of solid angle is
  Ω  =   A ∕r2
          -2
d Ω  =   r  dA
     =   r-2r2 sin θd θdφ

     =   sin θd θdφ                                   (18 )
The field of view of an instrument, e.g., a telescope, is most naturally measured by a solid angle.

The definition of ˉ
I ν (17) demands the radiation field be integrated over all angles, i.e., over all 4π steradians. Evaluating the denominator demonstrates the properties of angular integrals. The denominator of (17) is

∫          ∫ θ=π ∫ φ=2π
   dΩ  =               sin θdθ dφ
 Ω          θ=0   φ=0
                ∫ θ=π
       =   [φ]2π     sin θdθ
              0  θ=0
              ∫ θ=π
       =   2π       sin θdθ
               θ=0
       =   2π [-  cosθ]π0

       =   2π[- (- 1) - (- 1)]
       =   4π                                            (19 )
As expected, there are 4π steradians in a sphere, and 2π steradians in a hemisphere.

It is convenient to return briefly to the definition of isotropic radiation. Isotropic radiation is, by definition, equal intensity in all directions so that the total emitted radiation is simply 4π times the intensity of emission in any direction.

Applying (19) to (17) yields

         1 ∫
ˉIν  =   ---   Iν dΩ                               (20 )
        4π  Ω
Iˉν has units of radiance, W m-2 sr-1 Hz-1. If the radiation field is azimuthally independent (i.e., I ν does not depend on φ), then
          ∫
 ˉ      1-  π
Iν  =   2    Iν sin θd θ                             (21 )
           0

Let us simplify (21) by introducing the change of variables

 u  =   cosθ                                     (22 )

du  =   - sinθ dθ                                (23 )
This maps θ [0, π] into u [1,-1] so that (21) becomes
           ∫
ˉ         1-  -1
Iν  =   - 2     Iν du
          ∫ 11
ˉI   =   1-   I  du                                 (24 )
 ν      2  -1 ν

The hemispheric intensities or half-range intensities are simply the up- and downwelling components of which the full intensity is composed

Iν(τ,ˆΩ) = Iν(τ,θ,φ) = {   +
   Iν (τ, θ,φ)  :  0 < θ < π ∕2
   I-ν (τ, θ,φ)  :  π∕2 <  θ < π (25a)
Iν(τ,ˆΩ) = Iν(τ,u,φ) = {   +
   Iν- (τ, u,φ)  :  0 ≤ u <  1
   Iν (τ, u,φ)  :  - 1 < u < 0 (25b)

I+ ν (τ,μ,φ) = Iν(τ, +μ,φ) = Iν(τ, 0 < θ < π2) = Iν(τ, 0 < u < 1) (26a)
I- ν (τ,μ,φ) = Iν(τ, +μ,φ) = Iν(τ, π2 < θ < π) = Iν(τ,-1 < u < 0) (26b)

2.1.3 Irradiance

The spectral irradiance Fν measures the radiant energy flux transported through a given surface per unit area per unit time per unit wavelength. Although it is somewhat ambiguous, “flux” is used a synonym for irradiance, and has become deeply embedded in the literature [Madronich1987]. Consider a surface orthogonal to the Ωˆ direction. All radiant energy travelling parallel to ˆΩ crosses this surface and thus contributes to the irradiance with 100% efficiency. Energy travelling orthogonal to ˆΩ (and thus parallel to the surface), however, never crosses the surface and does not contribute to the irradiance. In general, the intensity Iν(ˆΩ) projects onto the surface with an efficiency cos Θ = Ωˆ ˆΩ , thus

        ∫
F   =      I cosθ dΩ
 ν       Ω  ν
        ∫ θ=π∫  φ=2π
    =               Iν cos θ sin θdθ dφ                     (27 )
         θ=0   φ=0
In a plane-parallel medium, this defines the net specific irradiance passing through a given vertical level. Note the similarity between (20) and (27). The former contains the zeroth moment of the intensity with respect to the cosine of the polar angle, the latter contains the first moment. Also note that (27) integrates the cosine-weighted radiance over all angles. If Iν is isotropic, i.e., Iν = I0 ν , then Fν = 0 due to the symmetry of cos θ.

Let us simplify (27) by introducing the change of variables u = cos θ, du = - sin θ dθ. This maps θ [0, π] into u [1,-1]:

        ∫      ∫
           u=-1   φ=2π
F ν  =                Iνu (- du) dφ
        ∫ u=1 ∫  φ=0
           u=1   φ=2π
     =               Iνu du dφ                            (28 )
          u=-1  φ=0

The irradiance per unit frequency, Fν, is simply related to the irradiance per unit wavelength, Fλ. The total irradiance over any given frequency range, [ν,ν + dν], say, is Fν dν. The irradiance over the same physical range when expressed in wavelength, [λ,λ - dλ], say, is Fλ dλ. The negative sign is introduced since -dλ increases in the same direction as +dν. Equating the total irradiance over the same region of frequency/wavelength, we obtain

F ν d ν =  - F λdλ
                dλ
   F ν  =  - F λ---
                d ν(  )
        =  - F λ-d-  c-
                d(ν   ν)
        =  - F    - c--
               λ    ν2
            c       λ2
   F ν  =   -2Fλ =  --F λ                            (29 )
            ν       c2
   F    =   c-F  =  ν-F                              (30 )
     λ      λ2 ν    c   ν
Thus Fν and Fλ are always of the same sign.

2.1.4 Actinic Flux

A quantity of great importance in photochemistry is the total convergence of radiation at a point. This quantity, called the actinic flux, FJ, determines the availability of photons for photochemical reactions. By definition, the intensity passing through a point P in the direction ˆ
Ω within the solid angle is Iν . We have not multiplied by cos θ since we are interested in the energy passing along ˆΩ (i.e., θ = 0). The energy from all directions passing through P is thus

        ∫
F J  =      I dΩ
 ν        4π ν
     =  4 πˉI                                     (31 )
            ν
Thus the actinic flux is simply 4π times the mean intensity ˉI ν (20). FJ ν  has units of W m-2 Hz-1 which are identical to the units of irradiance Fν (27). Although the nomenclature “actinic flux” is somewhat appropriate, it is also somewhat ambiguous. The “flux” measured by FJ ν at a point P is the energy convergence (per unit time, frequency, and area) through the surface of the sphere containing P . This differs from the “flux” measured by Fν, which is the net energy transport (per unit time, frequency, and area) through a defined horizontal surface. Thus it is safest to use the terms “actinic radiation field” for FJ ν and “irradiance” for Fν. Unfortunately the literature is permeated with the ambiguous terms “actinic flux” and “flux”, respectively.

The usefulness of actinic flux FJ ν becomes apparent only in conjunction with additional, species-dependent data describing the probability of photon absorption, or photo-absorption. Photo-absorption is the process of molecules absorbing photons. Each absorption removes energy (a photon) from the actinic radiation field. The amount of photo-absorption per unit volume is proportional to the number concentration of the absorbing species NA [m-3], the actinic radiation field FJ ν , and the efficiency with with each molecule absorbs photons. This efficiency is called the absorption cross-section, molecular cross section, or simply cross-section. The absorption cross-section is denoted by α and has units of [m-2]. In the literature, however, values of α usually appear in CGS units [cm-2]. To make the frequency-dependence of α explicit we write α(ν). If α depends significantly on temperature, too (as is true for ozone), we must consider α(ν,T).

The probability, per unit time, per unit frequency that a single molecule of species A will absorb a photon with frequency in [ν,ν + dν] is proportional to FJ ν (ν)α(ν)2 . Thus α(ν) is the effective cross-sectional area of a molecule for absorption. The absorption cross-section is the ratio between the number of photons (or total energy) absorbed by a molecule to the number (or total energy) per unit area convergent on the molecule. Let Fα ν [W m-3] be the energy absorbed per unit time, per unit frequency, per unit volume of air. Then

F αν (ν) =   NAF Jν (ν) α(ν)                            (32 )
where NA m-3 is the number concentration of A.

Photochemists are interested in the probability of absorbed radiation severing molecular bonds, and thus decomposing species AB into constituent species A and B. Notationally this process may be written in any of the equivalent forms

AB  + h ν  -→    A + B
           ν>ν0
AB  + h ν  -→    A + B
           λ<λ0
AB  + h ν  -→    A + B                              (33 )
Both forms indicate that the efficiency with which reaction (33) proceeds is a function of photon energy. The second form makes explicit that the photodissociation reaction does not proceed unless ν < ν0, where ν0 is the photolysis cutoff frequency. In any case, photon energy is conventionally written , rather than the less convenient hc∕λ.

The probability that a photon absorbed by AB will result in the photodissociation of AB, and the completion of (33), is called the quantum yield or quantum efficiency and is represented by φ. As a probability, φ is dimensionless3 . In addition to its dependence on ν, φ depends on temperature T for some important atmospheric reactions (such as ozone photolysis). We explicitly annotate the T -dependence of φ only for pertinent reactions. Measurement of φ(ν) for all conditions and reactions of atmospheric interest is an ongoing and important laboratory task.

The specific photolysis rate coefficient for the photodissociation of a species A is the number of photodissociations of A occuring per unit time, per unit volume of air, per unit frequency, per molecule of A. In accord with convention we denote the specific photolysis rate coefficient by Jν. The units of Jν are s-1 Hz-1.

        F-Jν (ν)α(-ν)φ(ν)
J ν  =        h ν
        4 πˉI (ν)α(ν)φ(ν)
     =  ----ν------------                            (34 )
               hν
The photon energy in the denominator converts the energy per unit area in FJ ν to units of photons per unit area. The factor of α turns this photon flux into a photo-absorption rate per unit area. The final factor, φ, converts the photo-absorption rate into a photodissociation rate coefficient. Note that each factor in the numerator of (34) requires detailed spectral knowledge, either of the radiation field or of the photochemical behavior of the molecule in question. This complexity is a hallmark of atmospheric photochemistry.

The total photolysis rate coefficient J is obtained by integrating (34) over all frequencies which may contribute to photodissociation

       ∫
J   =        J (ν)d ν
        ν> ν0  ν
       ∫       J
    =        Fν-(ν)α(ν)φ(ν)-dν
        ν> ν0       hν
       4 π∫     ˉI (ν)α(ν) φ(ν)
    =  ---      -ν------------d ν                        (35 )
        h   ν>ν0      ν
As mentioned above, evaluation of (35) requires essentially a complete knowledge of the radiative and photochemical properties of the environment and species of interest. Moreover, J is notoriously difficult to compute where there is any uncertainty in the input quantities.

Integration errors due to the discretization of (35) are quite common. To compute J with high accuracy, regular grids must have resolotion of ~1 nm in the ultraviolet, [Madronich1989]. Much of the difficulty is due to the steep but opposite gradients of FJ ν and φ which occur in the ultraviolet. High frequency features in α worsens this problem for some molecules.

The utility of J has motivated researchers to overcome these computational difficulties by brute force techniques and by clever parameterizations and numerical techniques [Chang et al.1987Dahlback and Stamnes1991Toon et al.1989Stamnes and Tsay1990Petropavlovskikh1995Landgraf and Crutzen1998Wild et al.2000]. It is common to refer to photolysis rate coeffients as “J-rates”, and to affix the name of the molecule to specify which individual reaction is pertinent. Another description for J is the first order rate coefficient in photochemical reactions. For example, JNO2 is the first order rate coefficient for

NO2  + h ν  λ<4-2→0nm  NO  + O                           (36 )
If [NO2] denotes the number concentration of NO2 in a closed system where photolysis is the only sink of NO2, then
d[NO2]-
  dt     =  - JNO2[NO2]  + SNO2                         (37 )
where SNO2 represents all sources of NO2. The terms in (37) all have dimensions of m-3 s-1. The first term on the RHS is the photolysis rate of NO2 in the system.

Figure 1 shows the spectral distribution of actinic flux in a clear mid-latitude summer atmosphere, and the absorption cross-section and quantum yield of NO2.


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Figure 1: (a) Spectral distribution of actinic flux FJ [# m-2 s-1 μm-1] at TOA and at the surface for a mid-latitude summer (MLS) atmosphere with a unit optical depth of dust or sulfate in the lowest kilometer. (b) Absorption cross section of NO2, αNO2 [m2 molecule-1]. (c) Quantum yield of NO2, φNO2 (36).

Figure 2 shows the vertical distribution of JNO2 [s-1] for the conditions shown in Figure (1).


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Figure 2: Vertical distribution of JNO2 [s-1] (36) for the conditions shown in Figure (1). (a) Absolute rates. (b) Rates normalized by clean sky rates.

In this section we have assumed the quantities FJ ν , α, and φ are somehow known and therefore available to use to compute J. Typically, α and φ are considered known quantities since they usually do not vary with time or space. Models may store their values in lookup tables or precompute their contributions to (35). The essence of forward radiative problems is to determine I~ν so that quantities such as Jν and Fα may be determined. In inverse radiative transfer problems which are encountered in much of remote sensing, both J and the species concentration are initially unknown and must be determined. We shall continue describing the methods of forward radiative transfer until we have tool