Soot Moments

The Soot Moments emission model uses Method of Moments formulation.

In the Method of Moments formulation, the r -th of up to four moments of the soot Particle Size Distribution Function (PSDF) is identified as M r .

The r'th moment of the PSDF is defined as:
Figure 1. EQUATION_DISPLAY
M r = i r i = 1 N i
(3670)

where N i is the number density of soot particles in the i'th (diameter) bin.

The zero-th moment is the total number density of all particles, whereas the first moment is proportional to the volume fraction of all soot particles. The soot particle sizes follow a distribution, or PSDF, and the second and third moments of this PSDF are the variance and skewness respectively.

The transport equation for the r -th moment is:

Figure 2. EQUATION_DISPLAY
( ρ M m r ) t + ∇⋅ [ ρ v M m r - ( μ σ + μ t σ t ) M m r ] = ω ˙ M r
(3671)

where M m r ( = M r / ρ ) is the mass-based moment, ρ is the gas density, σ is the soot molecular diffusivity (Schmidt number), σ t is the turbulent Schmidt number for soot, and ω ˙ M r is the average source term.

Soot Moment Source

The general soot moment source term ω ˙ M r is given by:
Figure 3. EQUATION_DISPLAY
ω ˙ M r = d M r d t
(3672)
where:
Figure 4. EQUATION_DISPLAY
d M r d t = R r + G r + W r
(3673)

where R r , G r , and W r are the instantaneous rates of particle nucleation, coagulation, and heterogeneous surface reaction terms (that is, surface growth, oxidation, and PAH condensation), respectively.

Based on the moments, the Soot characteristics are computed as follows:
Soot Number Density [ 1 / m 3 ]
Figure 5. EQUATION_DISPLAY
N = M 0 N A
(3674)
where M 0 is the zero-th moment and N A is Avogadro's number.
Soot Volume Fraction [no units]
Figure 6. EQUATION_DISPLAY
f v = M 1 M w s o o t ρ s o o t
(3675)
Soot Mass Density [ kg / m 3 ]
Figure 7. EQUATION_DISPLAY
M = M 1 M w s o o t
(3676)
Soot Mean Diameter [ m ]
Figure 8. EQUATION_DISPLAY
d = M 1 / 3 M 0 ( 6 M w s o o t π ρ s o o t N A ) 1 / 3
(3677)
Soot Surface Density [ m 2 / m 3 ]
Figure 9. EQUATION_DISPLAY
S = π N A M 2 / 3 ( 6 M w s o o t π ρ s o o t N A ) 1 / 3
(3678)
Nucleation Source
Particle nucleation (or particle inception) is an important first step in process of soot formation. Particle nucleation results in generation of the smallest sized soot particles. Nucleation is usually modeled as the coalescence of two PAH species (soot precursors) into a soot particle.
Single PAH Species Nucleation
For the single PAH species nucleation option, the soot precursor for inception is assumed to be pyrene (A4). If A4 is absent from the mechanism, an isomer with same chemical composition (C16H10) is used, such as A3R5. The nucleation rate for the moments is given as described by Frenklach et al. [786]:
Figure 10. EQUATION_DISPLAY
R 0 = ε 4 π k B T m C n C P A H d P A H 2 N P A H 2
(3679)
Figure 11. EQUATION_DISPLAY
R r = 2 n C P A H R r 1 r = 1 , 2 , ...
(3680)
where:
  • n C P A H is the number of carbon atoms per PAH molecule. For pyrene precursor (A4), n C P A H = 32 .
  • m C is the mass of a carbon atom (12.0).
  • d P A H is the diameter of the PAH molecule.
  • N P A H is the number density of the PAH molecules.
N P A H is based on the molar concentration of the PAH species which is obtained from the following quadratic equation, assuming a quasi-steady approximation for the PAH species:
Figure 12. EQUATION_DISPLAY
ω ˙ P A H = k p i [ P A H ] 2 + k c o n d [ P A H ]
(3681)
where ω ˙ P A H is the rate of formation of PAH from the A4 precursor, k p i represents the collision rate between the PAH molecules that form the first soot particle, and k c o n d represents the collision rate for the condensation of a PAH molecule on a soot particle.
C2H2 Nucleation
If the chemical mechanism used does not include A4 species, Simcenter STAR-CCM+ allows acetylene (C2H2) to be used as a soot precursor for nucleation. The expression for nucleation when using C2H2 as a soot precursor is given by:
Figure 13. EQUATION_DISPLAY
R r = 2 N A C min k N ( T ) [ C 2 H 2 ] r = 0
(3682)
For r = 1 , 2 , 3 :
Figure 14. EQUATION_DISPLAY
R r = 2 C min R r 1
(3683)
where:
  • N A is Avogadro's number.
  • C min is the number of carbon molecules in the smallest PAH which coagulates into a dimer to form the incipient soot particle—set as 10.
The expression for k N is given by:
Figure 15. EQUATION_DISPLAY
k N = 0.63 × 10 4 exp ( E A T )
(3684)
where E A = 21100 1/K.
Multi PAH Species Nucleation
Nucleation from multiple PAH-based species is modeled as the collision and coalescence of various gas-phase PAH species to form initial dimers.
To reduce the efficiency of the collisions between small PAH molecules, a sticking coefficient s C is used which is assumed to scale with the mass of the PAH molecules to the fourth power.
The rate of PAH dimerization is expressed as:
Figure 16. EQUATION_DISPLAY
ω ˙ dim e r = i s C ( 4 π k B T m i ) 1 / 2 ( 6 m i π ρ s o o t ) 2 / 3 [ P A H i ] 2
(3685)
where, m i is the mass of species i , k B is the Boltzmann constant, ρ s o o t is the soot density, T is the gas temperature, and [ P A H i ] is the concentration of PAH species i .
The sticking coefficients are as summarized below [784].
Species Name Chemical Formula Chemical Symbol Molecular Mass Sticking Coefficient
Naphthalene C10H8 A2 128 0.002
Acenaphthylene C12H8 A2R5 152 0.004
Biphenyl C12H10 P2 154 0.0085
Phenathrene C14H10 A3 178 0.015
Acephenanthrylene C16H10 A3R5 202 0.025
Pyrene C16H10 A4 202 0.025
Fluranthene C16H10 FLTN 202 0.025
Cyclopenta[cd]pyrene C18H10 A4R5 226 0.039
Removal of these dimers occurs by nucleation and condensation. Both the source terms for nucleation and condensation depend on the concentration of dimers which are assumed to be in quasi steady state. Thus, the dimer concentration is calculated as the solution of a quadratic equation given by:
Figure 17. EQUATION_DISPLAY
ω ˙ dim e r = β N [ dim e r ] 2 + i = 0 β C i N i [ dim e r ]
(3686)
where [ dim e r ] is the concentration of dimers, and N i is the number density of soot particles of class size i .
β N and β C i are collision rates given by [796]:
Figure 18. EQUATION_DISPLAY
β N = 2.2 16 π k B T m D d D 2
(3687)
Figure 19. EQUATION_DISPLAY
β C i = π k B T 2 μ D i ( d D + d c i ) 2
(3688)
where m D and d D are the mass and diameter of a dimer, respectively. μ D i is the reduced mass of a dimer and a soot particle, and d c i is the collision diameter of a soot particle.
The nucleation source term for the zeroth moment is then given by:
Figure 20. EQUATION_DISPLAY
R 0 = 1 2 β N [ D I M E R ] 2
(3689)

PAH Condensation Source

Some PAH molecules can condense on the soot particles. The source term due to PAH condensation is modeled as described in Frenklach and Wang [788].
Figure 21. EQUATION_DISPLAY
W r c o n d = 2.2 π k b T 2 m C Σ k = 0 r 1 ( r k ) ( C h 2 M r k + 1 2 P A H M k + 2 C h C s M r k P A H M k + 1 3 + C s 2 M r k 1 2 P A H M k + 2 3 )
(3690)
r = 1...4
k = 0... ( 1 r )
where d a is the collision diameter of PAH. Since only one class of PAH is assumed to condense onto the soot surface, the PAH moments in the expression above can be reduced to:
Figure 22. EQUATION_DISPLAY
M r P A H = m P A H r N P A H
(3691)
in Eqn. (3691), r can be replaced by either:
  • r k
  • r k + 1 2
  • r k 1 2

Coagulation Source

G r is evaluated by a double interpolation after inserting a mass-equivalent expression of the frequency rate of soot particle collision f . A general outline is presented here that is taken from Frenklach [787]. First, a grid function of order l in general form is defined as:
Figure 23. EQUATION_DISPLAY
f l ( x , y ) = Σ i = 1 Σ j = 1 ( m i + m j ) l m i x m j y ( m i 1 3 + m i 1 3 ) 2 N i N j l = 0 , 1 , 2 , ...
(3692)
Then the G r can be represented in terms of grid functions as:
Figure 24. EQUATION_DISPLAY
G 0 = 1 2 K f m M 0 2 f 1 2 ( 0 , 0 )
(3693)
Figure 25. EQUATION_DISPLAY
G r = 1 2 K f m M 0 2 Σ k = 1 r 1 ( r k ) f 1 2 ( k , r k ) r = 2 , 3 , ...
(3694)
Fractional-ordered grid functions can be obtained by Lagrange interpolation of integer ordered grid functions. For example:
Figure 26. EQUATION_DISPLAY
f 1 2 = f 0 3 8 f 1 3 4 f 2 1 8
(3695)
f l ( l = 0 , 1 , 2 , ... ) can be evaluated in terms of fractional-order moments through interpolation. For example, upon simplification:
Figure 27. EQUATION_DISPLAY
f 1 = 2 μ 13 6 μ 1 2 + 4 μ 11 6 μ 5 6 + 2 μ 3 2 μ 7 6
(3696)
where μ r and fractional-order reduced moment μ is obtained by interpolating whole-ordered moments. The coefficient K f m is given by:
Figure 28. EQUATION_DISPLAY
K f m = ε 6 k B T ρ s o o t ( 3 m C 4 π ρ s o o t )
(3697)

Surface Growth and Oxidation

Heterogeneous surface reactions, such as surface growth and oxidation, contribute to soot particle growth. It is generally accepted that acetylene (C2H2) is the main participating gas-phase species. In Simcenter STAR-CCM+, soot surface growth is modeled by either the surface Hydrogen-Abstraction-C2H2-Addition (HACA) mechanism, or the Hydrogen-Abstraction-Carbon-Addition-Ring-Closure (HACA-RC) mechanism.
HACA
The HACA mechanism (Appel et al. [781]) is summarized below:
Reaction Number Reaction
1 C s o o t H + H C s o o t + H 2
2 C s o o t H + O H C s o o t + H 2 O
3 C s o o t + H C s o o t H
4a C s o o t + C 2 H 2 C s o o t H + H
4b C s o o t + C 2 H 2 C s o o t + H
5 C s o o t + O 2 2 C O + p r o d u c t s
6 C s o o t + O H C O + p r o d u c t s
In these reactions, C s o o t H represents a reactive site on the surface of the soot particle, and C s o o t denotes the corresponding radical. The reaction rates are computed as Eqn. (3365).
The soot kinetic model parameters are given as (Appel et al. [781]):


The reactions with the gas-phase species are modeled as:
Figure 29. EQUATION_DISPLAY
W r C 2 H 2 = k 4 a [ C 2 H 2 ] α χ C s o o t π C s 2 M 0 Σ l = 0 r 1 ( r l ) μ l + 2 3 ( 2 ) r l
(3698)
Figure 30. EQUATION_DISPLAY
W r O 2 = k 5 [ O 2 ] α χ C s o o t π C s 2 M 0 Σ l = 0 r 1 ( r l ) μ l + 2 3 ( 2 ) r l
(3699)
Figure 31. EQUATION_DISPLAY
W r O H = γ O H [ O H ] π k B T 2 m O H N A C s 2 M 0 Σ l = 0 r 1 ( r l ) μ l + 2 3 ( 1 ) r l
(3700)
where:
  • α is the steric factor—the fraction of the soot surface sites available for reaction.
  • m O H is the mass of the OH radical.
  • γ O H is the collision efficiency for the OH radical.
The rate of the surface reaction depends on the particle surface area and the number of active reaction (radical) sites available. The number density of active radical sites can be obtained from the total number density of all radical sites on the soot surface using a steady-state approximation. The total number density of all radical sites is estimated to be 2.5 × 1015 cm-2.
Figure 32. EQUATION_DISPLAY
C s = ( 6 m C π ρ s o o t ) 1 3
(3701)
χ C s o o t is the number density of the surface radicals, given by:
Figure 33. EQUATION_DISPLAY
χ C s o o t = χ C s o o t H k 1 [ H ] + k 2 [ O H ] k 1 [ H 2 ] + k 2 [ H 2 O ] + k 3 [ H ] + k 4 a [ C 2 H 2 ] + k 5 [ O 2 ]
(3702)
where χ C s o o t is the nominal number density of the soot radical sites, for which a value of 2.3×1019 m−2 is prescribed. In the present work, the reaction pathway 4a from the table is considered, and 4b is ignored.
HACA-RC
The HACA-RC mechanism (Mauss et al. [794]) is summarized below:
Reaction Number Reaction
1a C s o o t , i H + H k 1 a C s o o t , i + H 2
1b C s o o t , i H + O H k 1 b C s o o t , i + H 2
2 C s o o t , i + H k 2 C s o o t , i H
3a C s o o t , i + C 2 H 2 k 3 a C s o o t , i C 2 H 2
3b C s o o t , i C 2 H 2 k 3 b C s o o t , i + 1 H + H
4a C s o o t , i + O 2 k 4 a C s o o t , i 1 + 2 C O
4b C s o o t , i C 2 H 2 + O 2 k 4 b C s o o t , i + 2 C H O
5 C s o o t , i H + O H k 5 C s o o t , i 1 + C H + C H O
In these reactions, C s o o t , i H represents a reactive site on the surface of the soot particle, and C s o o t , i denotes the corresponding radical. i and i + 1 denote the size classes.
In the first step, an H radical is abstracted from the soot surface by either an H or OH radical forming an active radical site that can in turn be deactivated by the addition of an H radical. An addition of acetylene follows that leads to the formation of a new aromatic ring. This step is assumed to be reversible (3b). The next two reactions (4a) and (4b) describe the oxidation of a radical site by molecular oxygen while the last reaction in the scheme describes the oxidation of an active (non-radical) site by an OH radical. Introducing a steady-state assumption for the radical sites C s o o t , i and C s o o t , i C 2 H 2 leads to an algebraic equation for their respective concentrations:
Figure 34. EQUATION_DISPLAY
[ C s o o t ] = ( k 1 a , f [ H ] + k 1 b , f [ H ] + k 5 [ O H ] k 1 a , b [ H 2 ] + k 1 b , b [ H 2 O ] + k 2 [ H ] + k 3 a , f [ C 2 H 2 ] f 3 , a + k 4 [ O 2 ] ) [ C s o o t ]
(3703)
Figure 35. EQUATION_DISPLAY
[ C s o o t C 2 H 2 ] = ( k 3 a , f [ C 2 H 2 ] k 3 b , f + k 3 a , b + k 4 , b [ O 2 ] ) [ C s o o t ]
(3704)
where:
Figure 36. EQUATION_DISPLAY
f 3 , a = k 3 b , f k 3 b , f + k 3 a , b + k 4 , b [ O 2 ]
(3705)
The concentration of active sites can be calculated by:
Figure 37. EQUATION_DISPLAY
[ C s o o t ] = Σ i = 1 α χ s o o t N A S i N i
(3706)
  • α is the steric factor—the fraction of the soot surface sites available for reaction.
  • χ s o o t is the number of surface sites per unit area.
  • N A is Avogadro's number.
  • S i is the surface area of size i .
  • N i is the number of particles of size i .
The rates of surface reactions for Eqn. (3703) to Eqn. (3706) are [798]:
Figure 38. EQUATION_DISPLAY
M ˙ r , s g = α k 3 a , f [ C 2 H 2 ] f 3 a A Σ k = 0 r– 1 ( r k ) M k + 2 / 3 Δ m r– k , r = 1 , 2 , ... s
(3707)
Figure 39. EQUATION_DISPLAY
M ˙ r , o x = α ( k 4 a [ O 2 ] A + k 5 [ O H ] ) Σ k = 0 r– 1 ( r k ) M k + 2 / 3 Δ m r– k , r = 1 , 2 , ... s
(3708)
The change of mass Δ m takes on the following values:
  • Δ m = 1 for surface growth
  • Δ m = 1 for oxidation
To describe the burnout of the smallest soot particles due to oxidation, the rate of the zero-th moment is corrected by:
Figure 40. EQUATION_DISPLAY
M ˙ r , o x = α ( k 4 a [ O 2 ] A + k 5 [ O H ] ) M 1 / 3
(3709)
The moment-independent pre-factors retrieved from the flamelet libraries are thus:
Figure 41. EQUATION_DISPLAY
P s g = α k 3 a , f [ C 2 H 2 ] f 3 a A
(3710)
Figure 42. EQUATION_DISPLAY
P o x = α ( k 4 a [ O 2 ] A + k 5 [ O H ] )
(3711)
where:
Figure 43. EQUATION_DISPLAY
A = ( k 1 a , f [ H ] + k 1 b , f [ H ] + k 5 [ O H ] k 1 a , b [ H 2 ] + k 1 b , b [ H 2 O ] + k 2 [ H ] + k 3 a , f [ C 2 H 2 ] f 3 , a + k 4 [ O 2 ] )
(3712)

In the HACA and HACA-RC mechanisms, the parameter α is difficult to quantify from a theoretical point of view and can have a marked influence on the soot levels. Steric factor α is defined as the fraction of the reactive sites ('armchair' sites) on the surface of the soot particle that are available for surface growth or oxidation reactions. The value of α ranges from zero to unity.

Various values and functional forms for α are found in literature. Simcenter STAR-CCM+ provides three ways to compute α : a constant value, a premixed temperature-based correlation, and as a user-defined scalar.

The premixed temperature-based correlation is taken from Appel et al. [781] who fitted the correlation for α , where α is a function of the local temperature and the average soot particle size, quantified by the reduced soot moment μ 1 , where μ 1 is calculated as:
Figure 44. EQUATION_DISPLAY
μ 1 = M 1 M 0
(3713)
Appel et al calculate α as:
Figure 45. EQUATION_DISPLAY
α = tanh ( a log μ 1 + b )
(3714)
where the fitted parameters are:

a = 12.65 0.00563 T

b = 1.38 + 0.00068 T

and