ences, which are due to the velocity field, using a Lagrangian .... on the right-hand ...... ____. 0.4. 0.8. 1.2. 1.0. 0.8. 0.6. 0.4. 0.2. 0.0. 0.0 o/, : \o o/,,2 = o.OOO4\o.
mt
I
lr
SA-Ca-44',S)
_WAROS
UNOERSTANDING I_JRBULENT SCALAR MIXING (lnalytical Services and Materials)
55
Unclas
p H1/34
0117772
--
.
D
_
_
=
_..
--
_._z_
T 7
--
L
°
- __.
=
w_
=
NASA
Contractor
Towards
Services
Hampton,
Virginia
Langley under
Mixing
_z Materials,
Inc.
for Research Contract
Center NAS1-18599
National Aeronautics Space Administration
and
Office of Management Scientific and Technical Information Program 1992
Scalar
S. Girimaji
Analytical
Prepared
4446
Understanding
Turbulent
Sharath
Report
Towards
understanding
scalar
turbulent
mixing Sharath A. S. & M. Inc.,
S. Girimaji Hampton,
Virginia
23666
Abstract In an effort
towards
understanding
turbulent
scalar
mixing,
we
study the effect of molecular mixing, first in isolation and then accounting for the effects of the velocity field. The chief motivation for this approach stems from the strong resemblance of the scalar probability density function (pdf) obtained from the scalar field evolving from the heat conduction equation and that evolving in a turbulent velocity different
field. However, the evolution for the two cases. We attempt
of the scalar dissipation is to account for these differ-
ences, which are due to the velocity field, using a Lagrangian analysis. After establishing the usefulness of this approach, the heat-conduction simulations (ItCS), in lieu of the more
frame we use expen-
sive direct numerical simulations (DNS), to study many of the less understood aspects of turbulent mixing. Comparison between the HCS data and available models are made whenever possible. It is established that the/3 pdf characterizes, quite well, the evolution of the scalar pdf during mixing from all types of non-premixed initial conditions.
1
Introduction
Diffusion and
of smoke
air in an aircraft
scalars
engineers
many
fices.
and
applications,
a detailed
scalar
(Pope
Pope
(1988)
turbulence.
sive scalar DNS also
and
apart
from
provide
model
(Chen,
strongly
model.
represents simplified
understanding
by DNS
data
of the
models
is the
study
equation
1991b). mixing
often of the
rather
use
process
than
mixing
Despite
The
(Girimaji
has
been
turbulent1992)
to formulate
importance recent
closure
1991a,
observations
these
These mixing,
1991)
leading
first
of pas-
1989).
mapping
Gao
of
density
studies
(Givi
as the
of practical
remains
used
DNS
1991,
emerged
of DNS
us the
of turbulent
models.
Pope
for scalar
for problems
(Girimaji
technique
has
direct
other
of the
(DNS)
pdf in constant
understanding
1989,
(pdf)
gave
reactions
mixing
and
model
of turbulent
A popular
of Burger's
Kraichnan
been
suf-
reaction,
simulations
henceforth)
chemical our
and
an instance
combustion
processes
enhancing
The/3-pdf
closure
with
bed for evaluating
Chen
validated
mixing
bulent
a test
mixing
have
of mixing
function
of the scalar
there
process.
by chemical
numerical
to as EP
in which
Environmental-
statistics
density
direct
of fuel
this mixing
is accompanied
The
mixing
instances
flow field.
basic
probability
then,
and
of numerous
of the
(referred
Since
atmosphere
in understanding
of the evolution
mixing
data,
two
mixing
1985).
the
in a turbulent
of the
close look at the details isotropic
but
a knowledge
when
is required and
are
diffused
understanding
Eswaran
into
alike are interested
However,
scalars
chimneys
engine
are convected
ists and For
from
such
as tur-
long strides,
our
incomplete.
in the
past
in related
Navier-Stokes).
to understand simpler In the
turbulent
systems same
vein,
(e.g.,
use
we first
study the evolution of initially-random scalar fields evolving according to the heat conductionequationrather than the full scalarevolution equation. Then weaccountfor the effectof the velocity field using a Lagrangianframe analysiswheretheseeffectsarerelated to the material-elementdeformation characteristicsof the turbulent velocity field. 1.1
Motivation
We study tion
the
evolution
of a scalar
field
¢(x, t) subject
to the
heat
conduc-
equation,
0¢
0_¢
--Ot = D--Ox_Ox_' rather
than
the
full evolution
equation,
0¢
where
D is the
field.
There
better
our
whether pdf
(F(¢))
several
understanding
the
scalar
02¢ = D--,OxiOxi
of Fickian a priori
turbulent
equation
¢ is the
conditional
probability-space
scalar
dissipation
same.
X(¢)
In either
to (Pope
t) is the such
a study
irrespective
(1) or (2), the case,
velocity
the
pdf
to of
scalarevolves
1985)
0_ aCa¢ value
X(¢)
For example,
to equation
field according
u(x,
to perform
mixing.
is the
(2) and
motivations
according
0F(¢) at where
diffusion
of turbulent
field evolves
evolution
in an isotropic
0¢
0--[ + ul--Oxi coefficient
are
(1)
(3)
{F(_/')x(_b)}' of the
is given
= D( ._-[¢ oxi(]xi
scalar
concentration
and
the
by
= ¢).
(4)
The notation (bit) is usedto denote the conditional expectation of respect
to r.
it is clear for the
For the
from
equation
diffusion
without
vation
that
the
pdf's
are
similar
quite
responding
values
principal
any
stage
of scalar
scalar
study
of the
scalar
rescaled
pdf,
to account
be assumed
of the
the velocity
of equation
a tilde
wavenumber
denotes vector
given
value
heat
in the
study
to be unity
can
study
is that
the
scalar
length
initial
scalar
easily
one
adopted
by
the
is, at shape
scale
and
tur-
we find
that
the
is quite
similar
to
by EP.
we first
scalar
understood
that
of variance,
study,
field in turbulent
cor-
That
length
decay
at the
scale.
variance,
to our
of equal-
here
shapes
equation
obser-
of scalar of EP
field obtained
As a prelude
our
case
be recalled
value
turbulent
be most
stages
DNS
of scalar
from
(for the
by the
conduction
of the velocity
field
(1)
It should
of the
field.
role
the
of the initial
the
pdf
velocity
from
DNS
comes
at various
characterized
from
scale-independent
equation
variance.
of the
At any
obtained
of the
obtained
is independent
0q_(k, t) Ot -
where
for this
condition)
decay
statistics. pdf
version
can
initial
are independent
pdf
to understand role
evolution
diffusivity
from
findings
pdf
Role
the
t can be simply
calculated
of scalar
scalar
the
the
motivation
to those
the
scalar
time
and
a posteriori
non-premixed
bulence
(3) that
coefficient
quantity,
of the
of analyzing
loss of generality.
A strong
of the
purpose
b with
from
attempt
mixing. the
The
spectral
(2),
v/L-T/_
the
rniffi(k-
Fourier
of magnitude
m,t)¢(m,t)dm-
transform k. From
of the
k2¢(k,t),
quantity
this equation
and
(5)
k is the
we can glean
that,
when the length scale of of the
scalar
field
(Is),
other
hand,
when
the
length
scale
smaller
is larger,
scales
until
the
the
physical
are
>> 1, the
effect
of the
velocity
velocity
are
diffusion
unaffected.
is such
velocity
latter
case
(l_,/Is 0), the
¢rnax < 1 and
¢,,i,_
values
are set
outside
In Figure
the
The
agreement
range
16
(¢,,,,,,
DNS
5, the
is compared
(a 2 > 0.05).
data
and
model,
of mixing
the DNS
of mixing
the
stages
and,
stages
between
fraction.
is probably
both
stages.
of mass
is
well with
latter
range
trend
M1 agrees
at the
of HCS
as a ratio
a 1283 simulation
intermediate
fraction.
decays
this
pdf and
accurate
model
consid-
dissipation
of the scalar
The
pdf
conditional
ratio
fraction
scalar
data
(when
to zero
the
of mass
for
(a = 0.1)
dissipation
HCS
X(¢)/X(0.5)
the early
range
Taking
is good
stage
and
as the
errors. DNS
early
of mass
the entire
and
conditional
DNS
to be statistically
comparison
dissipation
M2 over
The
Gaussianity
during
range
the
that
a 643 simulation.
DNS
a narrow
ditional and
from
fact
increases
the observed
HCS
the
over
of variance.
statistical
for the intermediate
of mixing,
the
with
between
adequate
constant
is minimum
due
agreement
and
is nearly
fraught
data
is only
normalized
con-
with
the
models
models
agree
with
During
the latter
is not Cmax).
as good. In the
The
middle
M1 HCS
stages HCS of the
range,the agreementis adequate,whereasneaxthe edges,it is poor. This disagreementnear the edgesof the range (¢mi,,,Cm_,)could be due to statistical error in HCS data. Nearthe edgesthe probability of _ is solow that at thesevaluesof massfraction there are very few samplesof scalar dissipation from which to computethe conditional dissipation. This statistical error makesit difficult to completely comprehendthe evolution of conditional dissipation at the edges.However,it can be surmisedfrom the earlier findings about Cm;,,(t)and ¢,_(t)
that the zero valuesof the conditional
dissipation migrate inwards (from 0 and 1) with increasedmixing. To circumvent the problem of too few statistical samplesat the edges of the scalar range, in Figure 6, we plot the fractional scalar dissipation, F{_)x(¢} £1
of the
HCS
data
is that
when
the statistical
dissipation
is weighted
'
quantity conditional Here,
the
agreement
between
is excellent.
The
is again
to the
scalar
due field.
yielding Apart dissipation than
the
the
scalar
jagged
With
smooth from
time,
along
suggests
that
nature
M1.
error
HCS of the
high
this
is high due the low probability,
the
advantage
by the
data
of very
the
of plotting
down
The
and
HCS-data
high
probability the
fl-pdf-based plot
at the
wavenumber
wavenumber
density
itself.
model earliest
components
components
M1 time
in the
die out
quickly,
the fractional
scalar
statistics. the
conditional
appears
model
the
presence
mathematical
is a physically
pdf
and
our
important
dissipation
(equation with
convenience
the efforts
3).
should
quantity.
alone, In fact,
probability
that the
density be
it offers,
directed
17
It is this determines
conditional function towards
quantity, the
rather
evolution
dissipation (equation modeling
of
always 27).
This
fractional
scalardissipation rather than conditional scalardissipation. Moreover,the valueof conditional dissipation outside the range (¢mi,_,Cm_,)is irrelevant. Our inferencesfrom Figures4 - 6 are 1. The conditional dissipation ratio, the
HCS,
2. The
and
normalized
M1 and ing.
model
M2 agree
too
large
is difficult always based
HCS
the statistical
to make
a valid
form
(as
¢ = 0.5 ¢,_,
both
that
the
to thin
down
(as suggested tend latter
fractional
with
is the
error
at the edges
the
more
dissipation
the early
For
normalized by
at long times
probable
scenario.
_
stages
of mix-
same
and
reason,
it
dissipation
Jiang
to a spike since
(Figure
of the
range
mapping-closure-
However,
mean
ratio,
this
asymptoting 1992).
DNS,
models
of the scalar
the
of O'Brien
time,
the
of the
conditional
suggested
by Girimaji
towards
X(¢)/X(0.5), during
model
from
well.
data
the
conditional-dissipation
if it tends
adequately
comparison.
whether
a constant
calculated
dissipation,
well with
to evaluate
has
M1 agree
conditional
At long times,
are
3. The
the
X(¢)/es,
HCS
1991),
or
shape
at
Cmi,, and
3), it appears
and
the
model
_$
M1 show the
2.3
excellent
scalar
agreement.
evolution,
Evolution
the
of scalar
Since
agreement
it is this quantity
that
determines
is of significance.
variance
and
mean
scalar
mean
scalar
dissipation
scales
are
dis-
sipation The
evolution
obtained
from
7. To precisely
of scalar HCS
variance
for various
understand
the
(a _) and initial
the
effect
length of the
18
velocity
field
plotted on the
(es)
in Figure evolution
of these
quantities,
of Eswaran between
and
the
HCS-es
we compare Pope
HCS
(1988,
and
decreases
a non-monotonic
scalar
dissipation
DNS
increases gradually
monotonic
behavior
is more
of HCS The
variance
above
discussed accounted
2.4
ities
of
scalar
gradient the
ks.
For all
However,
peaking,
then
more
for smaller DNS
mean
the mean
scalar
ks. The rate
DNS-es
DNS
rapidly.
decay
ks, the
the
For ks _< 4, the
After
the
biggest
of es.
as expected.
and
is that
Section,
scalar
This
non-
implication
of
is higher
than
is entirely
where
the
due
effects
to the of the
velocity
field,
velocity
is
field
are
initial
gradient
according
evolves
conditions
in the
according of these
scalar
functions.
to the
field,
In Figure
For
k8 = 16. times.
The
both
cases,
the
initial
8, the
Pope
(1988)
different.
evolution
approach
pdf
shown)
Eswaran
find that
normally
distributed.
This
log-normality
is discussed
in detail
in the
next
19
the
to discontinu-
field
is composed
flatness-factor
is, however, scalar
and
for ks = 8
Gaussian
is a consequence Section.
scalar
However,
is shown
moments
Gaussian.
Due
of the 0¢/0xl
(not
the
equation.
scalar-gradient
component the
equation,
heat-conduction
are quite
scalar-dissipation and
heat-conduction
to the fields
and
and
evolution
for small
which
of scalar-gradient
field
difference
pronounced
superskewness
long
12).
ks.
next
evolves
also
initial
of delta
11 and
The
data
for.
Pdf
If the
DNS
is in the
at first
phenomenon,
in the
the corresponding
in time,
evolution
for small
7 with
in the beginning.
decays,
that
data
evolution
dissipation
on the
Figures
monotonically
shows
this
Figure
dissipation of the
values far
at
from is log-
velocity
3
Accounting
In this Section, field
we attempt
on scalar
effect
effect
grangian field the
mixing.
simplifying
The
for the
assumptions
frame
Sections.
velocity
Let
the
(x,
velocity
coordinates
from
field t).
of the turbulent
previous
easily
Consider
U(X,
system
field
Section
velocity
are invoked
to
analysis.
as X, rather
coordinate
the
is most
field
of velocity
for the effect
in our
of reference
in a turbulent Eulerian
to account
Findings
of the
effects
the
t). than
accounted evolution
In this
Section,
x, as was
done
evolve
according
U[X(x,
t), t],
for in the of the
La-
scalar
we designate in the
previous
;_o
0X(x, t) cOt with
the
initial
-
(31)
condition,
x = x(o). The
velocity
Now,
field U(X,t)
let the
Eulerian
Lagrangian
system
coordinate according
evolves
system
according
coordinate
to the
system
X is nonstationary, following
(32)
curvilinear,
fluid particles,
the
Navier-Stokes
x be and
Cartesian. nonorthogonal.
scalar
concentration
equation. Then,
the In the
evolves
to cO¢(x, t) cOt -D
where
D is scalar
terms
of the
diffusivity.
Lagrangian
The
scalar
0¢(x,t) COt
cO2¢(X, t) cOXicOX_ '
molecular
diffusion
(33) can
be rewritten
in
derivatives:
-
COx_ coxb co2¢(x,t) D-_i cOX_ cOz_cOxb "
2O
(34)
The evolution equation of the pdf, ¢(x,
t) following
standard
methods
OG(¢,,t) Ot (In the (3)).
absence
the
(Pope
to the
Eulerian
It
the
time
value
findings
of scalar
that,
of the
can
only
the
concentration
be derived
using
the
velocity
field
pdf
modified
of the
concentration
shapes
velocity
pdf
to simplify has
during
a major the
(35)
to equation
scalar
Section
the
]¢ = ¢,)].
reduces
Lagrangian
previous
slightly
effect
equation
of the
while
averaged
scalar
field,
evolution,
for ks > 2 and the
the above
t) are identical.
F(¢,
scale
that
field,
pdf
found
field
scalar
Oxo Oxb O¢(x,t)O¢(x,t) Oxa Ozb
of the
was
unaltered implies
in an isotropic
isotropy
the
t), of the
1985):
of the velocity
Now we invoke (35).
particles
__r _m =-Do_p,O_,,tG_¢t't)(oXiOXi
Due
and
fluid
G(¢l,
Gt(¢t,
t)
equation effect
on
evolution
are
for ks _< 2. This,
we argue,
field
upon
is independent
conditioned
of the
scalar
value.
the That
is, we suggest
(0_o ozb O¢(x,t)O¢(x,t) ozo Oxb_O¢(x,t)O¢(x,t) _, ax, azo a_b I¢ = ¢,) _ (ax, ax," a_o axb I¢ = ¢,), (36) where fetched function
/°-_ °--_\ \ OXi
OXi
I
is independent
assumption,
since
of the initial
Subject
to the
OG(¢t,t) _ at _-D_ax,
the
scalar
above
of the value
scalar
of the
field. scalar
This
concentration
field, which is independent
assumption,
equation
is not
(35)
such
a far-
is a strong
of the velocity can be simplified
field. as
_____ Oxb 02 _Ozo 0¢(x, t) 0¢(x, t) I¢= ¢,)]. ox,'aCta¢,[a(f"t'( ax_ a_b (37)
21
Owing to the isotropy of the turbulencefield and the initial scalarfield, we can further simplify as follows: Ox_ Oxb _ =
(OX_Oxi'
(3s)
(-b-G_axe) - _obis).
Then,
Oa( ¢. t) Ot where
Xt(@)
is the
05 _ -(S>
Lagrangian
o_toc
conditional
= Now we suggest G(¢t,t) the
(and,
hence,
Lagrangian
field.
that
the
on
Rescaling
time
effect
pendent
seen
of the
scalar
of the
conduction
heat
be decoupled.
but
less so otherwise.
dissipation
dissipation
defined
as
[¢ = ¢')"
(40)
velocity
field on the
through
the
dissipation
scalar
evolution {S),
is independent
and
of the
of that
velocity
Z'
The
dissipation,
of a scalar
effects
these
coordinate
field evolving from
the
of molecular
simplifications
es.
time
T is inde-
velocity-field-independent
(1) alone,
the
(41)
in the
of a scalar
equation
Clearly,
dt,
evolution
field.
Thus,
can
scalar
pdf
dissipation
as the full problem.
Mean
the
velocity
scalar
(39)
as
that
conditional
of the is only
r = it is easily
scalar
Ox:
F(¢,t))
conditional
[G(¢t,t)xdCt)],
In isotropic
field can be approximated
Zt(¢l) under
same action
as (from
influence
initial and
will be accurate
turbulence,
the
the
is the
conditions
velocity
field
for ks > 2,
conditional
equations
36 and
3S) 0¢ 0¢ X(¢)
= (0---X, _-,
1¢ = ¢> = M 10
-4
I
10-5
l
I
0.04
O.O0
O.OB Time
102
101
.2 c
1
O°
t
_4
121
z_
0
4 M
D I
0 t_
A
I(1-I
a 4. 4
_ 44
8 io -2
+
o tO L/3
N N 10-3
10
4 0.00
I
I
I
0.04
I
0.08 Time
Figure 7i EvoluLion of IICS scalar variance and mean scalar dissipation tile case of # = 0.5. (Symbols same as in Figure 2.)
/44
for
18 16 &
&
&
&
6
&
_14
0 0
A
c 3
,0
_12 I
o
0
L
&
0
glO
0 O 0
_
8
O O _
A A
I _
6
5 o
4-
2
ooo o B 0
0_ 0.00
Elo o
rl
°°_°_°8
I
I
I
0.02
o o o
I
I
0.04
0.06
lime
Figure gradient
8:
Ev(,lution Odp/Oxl
Supcrskewncss:
of IlC, S flatness-factor (/t
--
0.5).
(Flatness
/x, _:, _- 16; 0 k, = 8.)
45
and factor:
super-skewness Q) k,
=
16;
of scalaro
k,
=
8.
5O
6
a 2 = 0.134
40
a 2 = 0.058
5 4
3e 3 20 2 '- \k%,. 10
1
0 ""--' 0.0
1
J
I,_==_
O.4
0 0.0
O.8
i 0.4
0.8
6
a 2 = 0.0 56
II=
5
:-_
4
C
c_3 "-
7_
CI U
ft.
0 0.0
I
0.4 Moss
0.8
Froclion
_,
#=0.,3
10
2O
8
16-
6
12-
4
8-
2
a 7 = 0.0005
4i
' 0.0
Figure represents
).4
of scalar data,
and
,)
0
0.8
9: Evolution ItCS
'
0.0
pdf, solid
F(¢), line
for the
represents/3-pdf
46
case
I
I
0.4
of in = 0.3. model
....
0.8
Dashed
calculations.
line
7 6 ,_
q,,,
/ ,'El
o
"4
.I/D
.6
q) to
2
1
I
0
I Illlll
I
I
]JHulll
1,
10-,3
10-4
0
Figure
I0:
Scalar
premixed
initial
0.20: (_(hezagon), model. /t = 0.40:
flatness-factor
I Ililll
I
(y
I
I Illl
10-I
10 0
2
vs.
conditions. O,
I
10-2
scalar
= 0.15:
]ICS; .... /3-pdf llC, S; - - -/3-pdf
variance
1:3, HCS; model. model.)
for
....
non-'equal
/3-pdf
/z = 0.30:
O,
model,
IICS;
nony =
--/3-pdf
60
f%
5O
t t l
O_
l (/1
4o
/
I:1
l
to C
El
! /
a,.
I
a) I
30
1
I:i
I /O
otrl
/"0
\
7
2O o ._.uo_d."--6'6-"
-
10
o
0
oO
o_
c_
"
0 10-4
Figure premixed
11:
Scalar initial
I I llllll
I
I
I lllll_
I0-3
vs.
(Symbols
scalar same
47
O"
(>... 0"_
I I IIIIII
10-2 (7 2
super-skewness conditions.
\ " "I_I
I llll
10-1
variance as Figure
10 0
for 10.)
non-equal
non-
2.0
_t
= 0.0056
5
1.6
__
4i 3
-._0.8
2
LL
1
0.4
o-:_ = 0.058
0.0
, 0.0 Moss
i O4
\"_"'. ,
Fraction
t
0 0,0
_z___ 0.8
0.4
I
0.8
_'J, /1.=0.5
12
20
a 2 = 0.0005
10
lo[
8 12 6 84 4-
2 O
0,0
Figure
12: Evolution model
of fractional
Dashed
line
') ).4
0.0
0.8
case of It = 0.3. fl-pdf
o
I
scalar
represents
dissipation, ItCS
calculations.
48
data
0.8
F(¢)X(¢)/e,, and
solid
line
for the represents
4.0 3.5 .3.0 2.5 t_
,,_ 2.0 1.5
1.0
0.5
0.0 0.0
0.2
0.4 Mass
Figure of/t
13: = 0.3.
Evolution HCS
of conditional
I 0.8
0.6
Froction0
scalar
data..
49
1.0
/_=0.3
dissipation,
X(4,)/¢,-,
for
the
case
12
12 10
a 2 = 0.201
8 6 4 2
o 0
0 0.0
0.4
0.8
0
0.0
4,0
0.4
0
0.8
3.0
..---,.
%3.5 2.5
I.L
_ 3.o
a_
= 0.130
_2
= 0.079
2.0
m 2.5 C o
2.0
-_
1.5 -
1.5 1.0 0.5
Q.
0.0 0.0
0.4 Moss
graclion
0.0 0.0
0.8 _,
tz=0.5
I
,
I
I
I
0,4 Mass
0.8
Fraction
1/_, #--0.5
0.4
0.8
3.0 2,5
7
_2 = 0.043
6 2.0 5 1.5
4
1.0
3 2
0.5 !. 0.0 0.0
Figure Case sents
14:
0,4
Evolution
0 0.0
0.8
of scalar
2 of subsection 4.2. Circles fl-pdf model calculations.
pdf,
F(¢,),
represent
5O
for partially-mixed tICS
data
and
initial solid
field,
line repre-
¢
4.Oh.
3.5
3.0
o,,o'b _.,
.. 0
2.5
_
_
U
I
vJ 2.0 In
¢1
_
1.5
1.0
0.5
0.0
|
I I IIIIIL__.]._t..I.L[|jI__I
lO-S
10-4
I IIllII
10-3
10-2
I
I I llIll
10-1
0 o
0 2 Figure
15:
initial 4.2,
flatness-factor
conditions. The
to cases the
Scalar
(O aud
solid
line
1 and
2.
corresponding
vs.
scalar
A represent
represents
tile
Q) ropresents mo(lel
HC$ /3-pdf
HCS
variance data
model
data
for
of Cases
partially-mixed
i and
calculations
of Case
2 of Section
corresponding
3, and
the
dashed
calculations.)
18 16
0
o_
0
0
0
14 o_. (/} r_ 0) C
12 10
,e, u'l
[
8 6 4 2 0
I
O-S
I I IIllll
I
I I IIIIII
10-4
I
initial
16:
Scalar
conditions.
super-skewness (Symbols
same
I
I I IIIiIl
10-2 o"
Figure
LJLIIIIII
10-3
vs.
I IIII
0 0
2
scalar
as Figure
51
I
10-1
variance 15.)
for
partially-mixed
line
REPORT P_k: r_ gathering
_
co_
04 kd'onna_on,
b_datl maJnlakl_
_lt.
BrAe
1204.
DOCUMENTATION
0ot 111_ _ ol _otrt_ltk_l ks 4mtJR_AId to athlK_ the d4Ma ne4l_. _nd con_olotir_ and t4wl_ng the kclud_;
Atilt.
suggeello_4 VA
_
2_2¢_-4302.
1. AGENCY USE ONLY (Leave b/ank,)
mduck_g
Ih,k; burden,
and to Ihe Offloe
TITLE
AND
| h_Jr _
to Washington
o( M_ma_
Form_prowd OMB No. 0704-0188
_ ml_OttN. |t_ud_ 0 11_ tkl_ 4_ inlor_M, Iovl. Send _
14eadq,.m,'tecs
_tcee.
and Budgeq. Papenvoqk
2. I:IEPORT DATE
July 4.
PAGE
1992
SUBTITLE
Dkeclorale Redu_lon
Project
kit rWvl41wk_ blltt_tk)414, s_chk_ r_N(b,t_ regatdk_g Ibis burdlk_ eltlmale 06' &ny othot for Inlormaflon
Opera=k)_;
(0704-01U).
Washln_on.
and R4potts. OC
1215
_ I_
soufc4l. o4 this
Je_wson
Davlg
20503.
3. REPORT TYPE AND DATES COVERED
Contractor Report 5.
FUNDING
NUMBERS
Towards Understanding Turbulent Scalar Mixing C NAS 1-18599 e. AUTHOR(S) Nll 505-62-40-06
Sharalh S. Girimaji
7. PERFORM=NO OROAN_.XTION NAME(S) AND,U>DRESS(ES) Analytical Services and Materials, Inc. 107 Research Drive Hampton, VA 23666
8. PERFORMING ORGANIZATION REPORT NUMBER
9. SPONSORING I MONITOR=NO AGENCy NAME(B) ANDADDRESS(ES) • National Aeronautics and Space Administration Langley Research Center Hampton, VA 23665-5225
10,
SPONSORING AGENCY
/ MONITORING
REPORT
NUMBER
NASA CR-4446
11. SUPPLEMENTARY NOTES Technical Monitor: J. Philip Drummond
12,. DIB'rRIBU'nON; AV,UL*BlUTY STATEMENT
12b. DISTRIBUTION CODE
Unclassified- Unlimited Subject Category 34
13. ABSTRACT (M_xlmum3OOw_)
In an effort towards understanding turbulent scalar mixing, we study the effect of molecular mixing, first in isolation and then accounting for the effects of the velocity lieU. The chief motivation for this approach stems from the strong resemblance of the scalar probability density function (pdf) obtained lrom the scalar field evolving from the heat conduction equation and that evolving in a turbulent velocity field. However, the evolution of the scalar dissipation is different for the two cases. We attempt to account for these differences, which are due to the veioctiy field, using a Lagrangian frame analysis. Afler establishing the usefulness of this approach, we use the heat-conduction simulations (HCS), in lieu of the more expensive direct numerical simulations (DNS), to study many of the less understood aspects of turbulent mixing. Comparison between the HCS data and available models are made whenever possible. It is established thai the Beta pdf characterizes, quite well, the evolution of the scalar pdf during mixing from all types of non-premixed initial conditions.
14. SUBJECT TERMS
15. NUMBER OF PAGES
turbulent-mixing models stochastic mixing
52 16. PRICE CODE
A04 17. SECURITY CLASSIFICATION OF REPORT
Unclassified NSN
7540-01-280-5500
18. SECURITY CLASSIFICATION OF THIS PAGE
lB. SECURITY CLASSIFICATION OF ABSTRACT
20. UMITATION OF ABSTRACT
Unclassified
Unlimited Standard F_rm 298 (Rev. 249) Pre_cdbed L_J- IG2
by A_NSI S_.
Z3g-18
NASA-Langley,
1992