∂z
∂Tw
∂z
- λs w
s
∂2 T
(17)
∂z2
in th e es timat ion of th ese values ar e not critical becau se th e operat ing conditions stu died here ar e below th e temperatur e region in which reaction with O2 becomes important 。
In regar ds to th e reaction with NO2, th e expe rimenta l data obta ined in th e engine tes ts will be used to fit th e two rat e param eters (activat ion energy an d preexpo- nent ial factor)。 The activat ion energy should be with in th e ran ge of values report ed in th e relat ed li teratur e。
Pressu re Drop Mode l。 The press ur e drop thr ough
th e soot layer is describe d by Darcy’s law with th e inclusion of th e nonlinear Forchh eimer term , which becomes important at high flow rat es。 In th e genera l case, th e different ial press ur e drop over a porous medi a of length dx is
dp ) µv + þFv2 (18) dx kp
Although th e ma ss flow rat e is steady thr oughout th e soot layer, th e gas velocity var ies along th e soot layer becau se of chan ges in th e gas density an d filtrat ion ar ea, as shown by th e cont inu ity equat ion
FwvwD
v(x) ) (19)
F(x) b(x)
The gas density var iat ion along th e soot layer is a function of th e local press ur e。 With th e ass um ption of ideal gas, th e density can be exp ressed as
p(x) M
lines of th e gas flow in th e filter in th e axial an d tran sverse directions。 Therefore, th e rat e of soot ac- cumu lat ion in each axial node along th e filter will be directly proport iona l to th e gas flow rat e at th e respe c- tive node in th e tran sverse direction。 Becau se th e solut ion of th e above balance equat ions provides th e tran sverse gas flow rat e distr ibut ion along th e filter chann el, it is stra ight forwar d to comput e th e rat e of soot accumu lat ion at each axial node。
Mode l Vali dation
The math emat ical model prese nt ed above still lacks
F(x) )
RT
(20)
th e informat ion on th e rat e param eters that describe th e NO2 reaction。 Neverth eless , by simu lat ing th e
Becau se of th e tra pezoidal sha pe of th e soot layer deposit, th e soot layer wid th increases as th e gas app roaches th e wall surface, according to th e followi ng relat ionship:
b(x) ) D - 2(w - x) (21)
The perm eability of soot is depe ndent on th e gas mean free path becau se of slip phenomena 。 This depe ndence can be exp ressed as26
engine tes ts, it is possible to obta in th e rat e constant s that produce good agreement betwee n expe riment an d simu lat ion。 A typical exam ple is prese nt ed in Figur e 5, which refers to an engine tes t consisting of six 10-min steady-stat e operat ing point s in series。
In a first step, it is necess ar y to ensur e that th e part iculat e filter temperatur e is predicted corr ectly thr oughout th e tes t。 This is obvious from th e uppe r gra ph, which compar es th e measur ed an d comput ed temperatur es at th e filter exit。 It ha s to be ment ioned that th e heat of th e NO2 reaction at th ese operat ing
p0
kp ) k0 1 + C µ
T (22)
conditions produces negligible temperatur e chan ges in th e filter。 In fact, almost isoth erma l conditions occur 柴油机碳烟氧化英文文献和中文翻译(12):http://www.youerw.com/fanyi/lunwen_99285.html