notes lecture 2 - princeton university · (bird, stewart & lightfoot) rx 1 = x 1x 2 y 1y 2 ry 1...
TRANSCRIPT
Summer 2013
Moshe Matalon University of Illinois at Urbana-‐Champaign 1
Lecture 2 Constitutive Relations
Moshe Matalon
⇢De
Dt= �pr · v + ��r · q
⇢Dh
Dt=
Dp
Dt+ ��r · q
⇢Dv
Dt= �rp+r ·⌃+ ⇢g
⇢DYi
Dt+r · (⇢YiVi) = !i i = 1, 2, . . . , N
@⇢
@t+r · ⇢v = 0
h =NX
i=1
Yi
ho
i
+
ZT
T
o
cp
dT
We already have expressions for the viscous stress tensor ⌃ and the dissipa-
tion function �. We need constitutive relations for the heat flux vector q, thedi↵usion velocities Vi and the rates of consumption/production !i.
Conservation equations
p = ⇢RTNX
i=1
Yi
Wi
{
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q = ��rT + ⇢NX
i=1
YihiVi + qR
The total energy flux q is the sum of the separate energy fluxes, including the
fluxes due to di↵usion and the radiant flux qR , but neglecting the Dufour heat
flux (due to di↵erence in di↵usion velocities)
Heat flux vector
⇢Dh
Dt=
Dp
Dt+ �+r · (�rT )�r ·
NX
i=1
⇢YiVihi
Radiative heat transfer will also be removed and added only when necessary.
⇢Dh
Dt=
Dp
Dt+ �+r · (�rT )�r ·
NX
i=1
⇢YiVihi
| {z }the energy transfer is not
just by conduction, but also
through di↵usion fluxes
of the di↵erent species
�r · qR
Moshe Matalon
h =NX
i=1
Yi
ho
i
+
ZT
T
o
cp
dT
⇢Dh
Dt=
Dp
Dt+ �+r · (�rT )�r ·
NX
i=1
⇢YiVihi
⇢D
Dt
ZT
T
o
cp
dT +NX
i=1
⇢DY
i
Dtho
i
r ·NX
i=1
⇢Yi
Vi
[ho
i
+
ZT
T
o
cp
i
dT ]
r ·NX
i=1
⇢Yi
Vi
ho
i
+r ·NX
i=1
⇢Yi
Vi
ZT
T
o
cp
i
dT
⇢D
Dt
ZT
T
o
cp
dT =Dp
Dt+ �+r · (�rT )�
NX
i=1
✓⇢DY
i
Dt+r·⇢Y
i
Vi
◆
| {z }!
i
ho
i
�r ·NX
i=1
⇢Yi
Vi
ZT
T
o
cp
i
dT
⇢D
Dt
ZT
T
o
cp
dT
!=
Dp
Dt+�+r · (�rT )�r ·
NX
i=1
⇢Yi
Vi
ZT
T
o
cp
i
dT �NX
i=1
!i
ho
i
(I)
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⇢Dh
Dt=
Dp
Dt+ �+r · (�rT )�r ·
NX
i=1
⇢YiVihi
⇢cpDT
Dt+
NX
i=1
hi⇢DYi
Dt=
Dp
Dt+ �+r · (�rT )�r ·
NX
i=1
⇢YiVihi
⇢cpDT
Dt=
Dp
Dt+�+r·(�rT )�
NX
i=1
⇢YiVi·rhi�NX
i=1
hi
⇢DYi
Dt+r · (⇢YiVi)
�
| {z }!i
h =NX
i=1
hiYi ) dh =NX
i=1
dhiYi +NX
i=1
hidYi
=NX
i=1
cpiYidT +NX
i=1
hidYi = cpdT +NX
i=1
hidYi
) Dh
Dt= cp
DT
Dt+
NX
i=1
hiDYi
Dt
Alternative form of the energy equation
Moshe Matalon
hi
= ho
i
+
ZT
T
o
cp
i
dT ) rhi
= cp
i
rT
⇢cpDT
Dt=
Dp
Dt+ �+r · (�rT )�
NX
i=1
⇢YiVi ·rhi �NX
i=1
hi!i
(II)
and it can be shown that the two versions are equivalent. Moreover, when all
the cpi are the same, i.e., cpi = cp for all i, the energy equation reduces to
⇢cp
DT
Dt=
Dp
Dt+ �+r · (�rT )�
NX
i=1
ho
i
!i
⇢cpDT
Dt=
Dp
Dt+ �+r · (�rT )�
NX
i=1
⇢cpiYiVi ·rT �
NX
i=1
hi!i
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Di↵usion
In a binary mixture Fick’s law of di↵usion states that the di↵usion mass flux of
a given species is proportional to its concentration gradient
⇢Y1V1 = �⇢D12 rY1
⇢Y2V2 = �⇢D21 rY2
⇢DYi
Dt+r · (⇢YiVi) = !i i = 1, 2
⇢YiVi = �⇢DrYi
⇢DYi
Dt+r · (⇢DrYi) = !i i = 1, 2
For ⇢D = const. )
Fick’s law of binary di↵usion
The constrains Y1V1 + Y2V2 = 0, and Y1 + Y2 = 1, imply that D12 = D21 ⌘ D
DYi
Dt+Dr2Yi = !i i = 1, 2
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(Curtiss & Hirschfelder 1949)
rXi =NX
j=1
XiXj
Dij(Vj �Vi)
| {z }di↵erence in
di↵usion velocities
+(Yi �Xi)rp
p| {z }pressure
gradient
+NX
j=1
XiXj
⇢Dij
DT
j
Yj� DT
i
Yi
!rT
T| {z }
temperature gradient
Soret e↵ect
+⇢
p
NX
j=1
YiYj(fi � fj)
| {z }di↵erence in
body force
Stefan-Maxwell equations
rXi =NX
j=1
XiXj
Dij(Vj �Vi)
For multicomponent di↵usion in gases
The e↵ects of pressure gradients, and temperature gradients (known as Soret
e↵ect) on di↵usion are typically small. If, in addition, there are no significant
unequal forces acting on the species (often relevant for ions and electrons where
f is due to an electrical field), then
where Dij are the binary di↵usivities, which have been proven to be sym-
metric, i.e., Dij = Dji. For a dilute ideal gas mixture they are independent of
composition, and determined by a simple two-components experiment where a
species in low concentration di↵uses through a second species that is in abun-
dance.
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rX1 =X1X2
D12(V2 �V1)
rX2 =X2X1
D21(V1 �V2)
)
and the Stefan-Maxwell equations reduce to Fick’s law of di↵usion
r(X1 +X2)
X1X2= (V2 �V1)
✓1
D12� 1
D21
◆= 0
Y1V1 = �DrY1
Y2V2 = �DrY2
D12 = D21 ⌘ D
More generally, Fick’s law is recovered if one assumes that the binary di↵usion
coe�cients are all equal, i.e., Dij = D.
YiVi = �DrYi for i = 1, . . . , N
For a binary mixture
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rXi =NX
j=1
XiXj
Dij(Vj �Vi) =
Xi
D
NX
j=1
Xj(Vj �Vi) =Xi
D
NX
j=1
XjVj �Xi
D Vi
DrXi
Xi=
NX
j=1
XjVj �Vi
D✓rYi
Yi+
rW
W
◆= DrW
W�Vi
YiVi = �DrYi
Xi = WYi/Wi ) rXi
Xi=
rYi
Yi+
rW
W
If the binary di↵usion coe�cients are all equal, i.e., Dij = D, we again cover
Fick’s law.
DrXi
Xi= DrW
W�Vi
it can be shown, after some algebraic manipulations that
PNj=1 XjVj = D(rW/W )
and, since
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The use of the Stefan-Maxwell equations is quite complicated because the dif-
fusion velocities Vi are not expressed explicitly in terms of the concentration
gradients.
NX
i=1
YiDij = 0 for all j
Vi =NX
j=1
Dij rXj
Generalized Fick equations
The coe�cients Dij , which don’t have to be necessarily positive, satisfy
Dij = Dji, for all i, j
would be more convenient for the evaluation of the di↵usion term in the species
equations, but the ”Fick di↵usivities” Dij are not simply related to the binary
di↵usivities Dij , and they are concentration-dependent.
Note that there are many definitions for multicomponent di↵usivities; the one
quoted here (with the Dij symmetric) follow Curtiss & Bird (1999).
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Stefan-Maxwell
V1 = D11rX1 +D12rX2
V2 = D21rX1 +D22rX2
Multi-component di↵usion
D12 = D21D11Y1 +D12Y2 = 0
D12Y1 +D22Y2 = 0
D12 = D21
One can find the relation between the multi-component di↵usivities Dij and thebinary di↵usivities Dij . For a binary mixture
rX1 =X1X2
D12(V2 �V1)
rX2 =X1X2
D21(V1 �V2)
D11 = � Y22
X1X2D12
D22 = � Y12
X1X2D12
D12 = D21 =Y1Y2
X1X2D12
)
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Expressions for ternary and quaternary mixtures are available, but are more
complicated.
D11 = �(Y2+Y3)
2
X1D23+ Y2
2
X2D13+ Y3
2
X3D12
X1D12D13
+ X2D12D23
+ X3D13D23
D12 =Y1(Y2+Y3)
X1D23+ Y2(Y1+Y3)
X2D13� Y3
2
X3D12
X1D12D13
+ X2D12D23
+ X3D13D23
with the additional entries generated by cyclic permutation of the indices.
For the general case, one can write a relation between the matrix of Fick di↵u-
sivities Dij and that of binary (Stefan-Maxwell) di↵usivities Dij ; see Curtiss &
Bird Ind. Eng. Chem. Res. 38:2515-2522 (1999).
For example, for a ternary mixture
Moshe Matalon
Vi =NX
j=1
D̂ij rYj
We are interested in rewriting the generalized Fick equations in terms of the
mass fraction
rXi = �W 2
Wi
NX
j=1j 6=i
1
W+ Yi
✓1
Wj� 1
Wi
◆�rYj .
This leads, in general to complicated expressions for the
ˆDij .
which requires expressing rXi in terms of rYi, or using the di↵erential relation
(Bird, Stewart & Lightfoot)
rX1 =X1X2
Y1Y2rY1 rX2 =
X2X1
Y2Y1rY2
For a binary mixture,
D̂11 = �Y2
Y1D D̂22 = �Y1
Y2D D̂12 = D̂21 = D
and we recover Fick’s law, as we should.
Y1V1 = �DY2rY1 +DY1rY2 = �D(Y2 + Y1)rY1 = �DrY1
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Yi ⌧ 1 for i = 1, · · · , N � 1, YN ⇠ 1
Xi ⌧ 1 for i = 1, · · · , N � 1, XN ⇠ 1
W =NX
i=1
XiWi ⇠ WN
NX
i=1
YiVi = 0, ) VN ⌧ 1
YiVi = �Di rYi for i = 1, 2, · · · , N � 1
Dilute mixture
There is an abundant species in the mixture, denoted by N , while all other
species may be treated as trace species (for combustion in air, nitrogen is abun-
dant)
rXi =
NX
j=1
XiXj
Di,j(Vj �Vi) ⇠ �XiVi
Di,Nfor i = 1, 2, · · · , N � 1
rYi ⇠ �YiVi
DiNfor i = 1, 2, · · · , N � 1
Fick’s law may be used as an approximation with the di↵usion coe�cient inter-
preted as the binary di↵usion coe�cient with respect to the abundant species,
i.e., Di = DiN . The equation for N is still complicated, but is not needed
because YN = 1�PN�1
i=1 Yi Moshe Matalon
note, however, that this can be only used forN�1 species, with the last obtained
from the constrain
PYiVi = 0.
YiVi = �Di,e↵rYi or XiVi = �Di,e↵rXi
rXi =NX
j=1
XiXj
Di,j(Vj �Vi) ⇡ �
NX
j=1
XiXj
Di,jVi = �XiVi (
Xi
Di,e↵+
NX
j=1j 6=i
Xj
Dij)
�XiVi
Di,e↵⇡ �XiVi (
Xi
Di,e↵+
NX
j=1j 6=i
Xj
Dij)
Di,e↵ =1�Xi
NPj=1j 6=i
Xj/Dij
A useful approximation is the e↵ective binary di↵usivity for the di↵usion of
species i in the mixture, obtained by assuming that Vj ⇡ 0 for all the species,
except for Vi 6= 0.
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⇢D
Dt
ZT
T
o
cp
dT
!=
Dp
Dt+�+r·(�rT )+r ·
NX
i=1
⇢Di
rYi
ZT
T
o
cp
i
dT
!
| {z }�
NX
i=1
!i
ho
i
⇢D
Dt
ZT
T
o
cp
dT
!=
Dp
Dt+�+r·(�rT )�r·
NX
i=1
⇢Yi
Vi
ZT
T
o
cp
i
dT
!�
NX
i=1
!i
ho
i
Introducing the di↵usion law YiVi = �Di rYi in the energy equation
If Di = D for all i
energy transfer due to di↵usion
fluxes caused by imbalances in the
di↵usivities and specific heats.
⇢D
Dt
ZT
T
o
cp
dT
!=
Dp
Dt+�+r·(�rT )+r·⇢D
NX
i=1
rYi
ZT
T
o
cp
i
dT
!
| {z }�
NX
i=1
!i
ho
i
NX
i=1
rYi
Z T
T o
cpidT
!= r
NX
i=1
Yi
Z T
T o
cpidT
!�
NX
i=1
Yir Z T
T o
cpidT
!
= rNX
i=1
Yi
Z T
T o
cpidT �NX
i=1
YicpirT = rNX
i=1
Yi
Z T
T o
cpidT � cprT =
z }| {
rZ T
T o
cpdT � cprT
Moshe Matalon
r · ⇢D rZ T
T o
cpdT � cprT
!
⇢D
Dt
ZT
T
o
cp
dT
!=
Dp
Dt+�+r·(�rT )+r · ⇢D
NX
i=1
rYi
ZT
T
o
cp
i
dT
!
| {z }�
NX
i=1
!i
ho
i
⇢cp
DT
Dt�r · (�rT ) =
Dp
Dt+ ��
NX
i=1
!i
ho
i
⇢D
Dt
ZT
T
o
cp
dT
!�r ·
"⇢Dr
ZT
T
o
cp
dT + �⇣1� ⇢Dc
p
�
⌘
| {z }rT
#=
Dp
Dt+ ��
NX
i=1
!i
ho
i
= 0 whenD = �/⇢cp
When all the cpi are also the same, cpi=cp=cp(T ) for all i, the energy equation
reduces to
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Governing Equations
with Fickian di↵usion (dilute mixture) and equal cpi
@⇢
@t+r · ⇢v = 0
⇢Dv
Dt= �rp+r · µ[(rv)+(rv)T] +r(� 2
3µ)(r · v) + ⇢g
⇢DYi
Dt�r · (⇢DirYi) = !i, i = 1, 2, . . . , N � 1
⇢cp
DT
Dt�r · (�rT ) =
Dp
Dt+ ��
NX
i=1
!i
ho
i
Moshe Matalon
Transport Coe�cients
The bulk viscosity is negligible in combustion processes; ⇡ 0.
⌃ = µ[(rv) + (rv)T]� 2
3µ(r · v)I
� =1
2µ
✓@vi
@xj+
@vj
@xi
◆2
� 2
3µ(r · v)2
Although the transport coe�cients �, µ in a multicomponent mixture depend in
general on the concentrations, this dependence is generally ignored in theoreti-
cal studies and average quantities are used; they remain dependent on pressure
and temperature.
Similarly W is taken as constant, so that the equation of state reduces to
p = ⇢RT/W .
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The thermal conductivity depends mostly on temperature, and behaves as
� ⇠ T↵/p with 1/2 ↵ 1. More relevant, however, is the thermal di↵u-
sivity �/⇢cp which has the same units and the same temperature and pressure
dependence as the molecular di↵usivities and the kinematic viscosity. In partic-
ular
�/⇢cp ⇠ T↵/p 3/2 ↵ 2
Typical values at p = 1atm are in the range 0.1� 1 cm2/s.
The dependence of the binary di↵usivities Di on pressure and temperature is
Di ⇠ T↵/p 3/2 ↵ 2
Typical values at p = 1atm are in the range 0.01� 10 cm2/s.
µ/⇢ ⇠ T↵/p 3/2 ↵ 2
Typical values at p = 1atm are in the range 0.1� 1 cm2/s.
The kinematic viscosity µ/⇢ has the same units and the same pressure and tem-
perature dependence as the molecular di↵usivities
Moshe Matalon
Since �/⇥cp, µ/⇥,Di have the same dependence on temperature, their ratios are
nearly constant.
We can write ⇢Di = Le
�1i (�/cp) and µ = Pr(�/cp) with � = �(T ). A good
approximation (Smooke & Giovangigli, 1992) for the latter is
�
cp= 2.58 · 10�4
✓T
298K
◆0.7g
cm s
The Prandtl and Lewis numbers are nearly constant; Pr = 0.75 and for common
combustible mixtures Le varies in the range 0.2� 1.8.
�/⇥cpDi
= Lei
µ/⇥
�/⇥cp= Pr
µ/�
Di= Sci Schmidt number
Prandtl number
Lewis number
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p = �RT/W
�Dv
Dt= �⇥p+ µ
⇥⇥2v + 1
3⇥(⇥ · v)⇤+ �g
⇥�
⇥t+� · �v = 0
If the transport coe�cients µ,�, ⇢Di assume constant values (an average value,
say) the equations simplify to
⇢cp
DT
Dt� �r2T =
Dp
Dt+ ��
NX
i=1
!i
ho
i
⇢DYi
Dt� ⇢Dir2Yi = !i, i = 1 . . . N � 1
there are N+6 variables (�, p, T,v, Yi) and N+5 equations, supplemented with
the constrain
PNi=1 Yi = 1.
Moshe Matalon