scieee Science in your language
[en] (orig)

Steady uniform shear flow in a low density granular gas

Abstract

The steady uniform shear flow of a low density granular sytem is studied by means of a kinetic model equation and also by direct Monte Carlo simulation of the Boltzmann equation. The former can be exactly solved for arbitrary shear rate and dissipation. Explicit expressions for the one-particle distribution function and the pressure tensor are obtained. Comparison of the results with those of previous theories is presented in the appropriate limits. The simulation shows that the model reproduces fairly well the values of the stresses and, in particular, the phenomenon of normal stress differences. The agreement is also very good for the velocity distribution function in the thermal velocity region, although significant discrepancies appear for large velocities.

Read accessible full text

Steady uniform shear flow in a low density granular gas

Author: Brey Abalo, José Javier; Ruiz Montero, María José; Moreno Franco, Francisco
Publisher: American Physical Society
Year: 1997
DOI: 10.1103/PhysRevE.55.2846
Source: https://idus.us.es/bitstreams/b5c1b0ca-d68e-4254-8bb2-d9e5da41ab37/download
S eady uni o m shea low in a low densi y g anula gas
J. J. B ey, M. J. Ruiz-Mon e o, and F. Mo eno
Fı
´sica Teo
´ ica, Facul ad de Fı
´sica, Uni e sidad de Se illa, Apa ado de Co eos 1065, E-41080 Se illa, Spain
~Recei ed 8 Oc obe 1996!
The s eady uni o m shea low o a low densi y g anula sy em is s udied by means o a kine ic model
equa ion and also by di ec Mon e Ca lo simula ion o he Bol zmann equa ion. The o me can be exac ly
sol ed o a bi a y shea a e and dissipa ion. Explici exp essions o he one-pa icle dis ibu ion unc ion
and he p essu e enso a e ob ained. Compa ison o he esul s wi h hose o p e ious heo ies is p esen ed in
he app op ia e limi s. The simula ion shows ha he model ep oduces ai ly well he alues o he s esses
and, in pa icula , he phenomenon o no mal s ess di e ences. The ag eemen is also e y good o he
eloci y dis ibu ion unc ion in he he mal eloci y egion, al hough signi ican disc epancies appea o la ge
eloci ies. @S1063-651X~97!12803-3#
PACS numbe ~s!: 05.20.Dd, 47.50.1d, 47.20.2k
I. INTRODUCTION
The de elopmen o kine ic model equa ions desc ibing
he dynamics o pa icles, which collide inelas ically, seems
o be an impo an s ep owa ds he unde s anding o he
complex phenomena aking place in apid g anula lows
@1–3#. Ne e heless, he nonconse a ion o ene gy in colli-
sions in oduces qui e d as ic changes in he physics o he
p oblem, and he gene aliza ion o he exis ing heo ies o
o dina y luids is a om being an easy ask. This e e s o
bo h he own de i a ion o p oposal o a kine ic equa ion o
he dis ibu ion unc ion o he sys em and also o sol ing he
equa ion o ob ain consis en hyd odynamic-like equa ions
desc ibing he mac oscopic e olu ion. Al hough a hyd ody-
namic desc ip ion, in e ms o he densi y, he mac oscopic
low eloci y, and he g anula empe a u e is sugges ed by
analogy wi h no mal luids and also by expe imen s and
compu e simula ions, a de i a ion om a mo e undamen al
desc ip ion o he sys em is needed.
In he las yea s, se e al kine ic equa ions o he one-
pa icle dis ibu ion unc ion o apid g anula lows ha e
been p oposed, ex ending he heu is ic a gumen s leading o
he Bol zmann and Enskog equa ions o o dina y gases
@4–7#. In addi ion, a mo e basic app oach o he p oblem,
s a ing om he Liou ille equa ion, has been p esen ed @8#.
Ne e heless, e en i i is assumed ha hese equa ions a e
ele an o he desc ip ion o apid g anula lows, a unda-
men al di icul y a ises. The s anda d p ocedu e o ob aining
solu ions o kine ic equa ions is by means o he Chapman-
Enskog me hod @9#, in which an expansion in he g adien s
o he hyd odynamic ields is ca ied ou . Fo molecula lu-
ids, he e e ence s a e abou which g adien s a e conside ed
is he Maxwellian local equilib ium dis ibu ion. The co e-
sponding e e ence dis ibu ion o inelas ic pa icles is com-
plex and has no been de e mined o da e. As a consequence,
he limi o small dissipa ion ~i.e., he coe icien o es i u-
ion
a
close o 1!is usually conside ed. Ne e heless, many
o he phenomena peculia o apid g anula luids a e clea ly
associa ed o nonlinea and heological e ec s and o no
e y small dissipa ion. This includes p ope ies such as sig-
ni ican no mal s ess di e ences unde shea @2,10,11#,
spon aneous o ma ion o dense clus e s su ounded by e-
gions o low densi y @12–15#, and inelas ic collapse @13#.
The easons men ioned abo e indica e ha i is ins uc i e
o conside simple model kine ic equa ions o inelas ic gases
which allow con olled and de ailed analysis. Kine ic models
ha e p o en o be e y use ul in he s udy o a om equi-
lib ium s a es o dilu e molecula gases @16#. Fo many
physical si ua ions, exac solu ions o he models ha e been
de i ed, and compa ison wi h nume ical solu ions o he ex-
ac equa ions ob ained by compu e simula ion shows a ai ly
good ag eemen . Ve y ecen ly @8#, wo kine ic models o
sys ems o inelas ic ha d sphe es ha e been p oposed. Bo h
models a e o mula ed as app oxima ions o he e ised En-
skog equa ion, bu wi h di e en quan i a i e accu acy. He e
we will conside he limi o low densi ies and la ge leng h
scales as compa ed wi h he diame e o he pa icles. In his
limi , he wo models lead o he same equa ion, and become
a kine ic model o he Bol zmann equa ion o inelas ic ha d
pa icles.
Mos o he simples a om equilib ium physical si ua-
ions co espond o s eady s a es. In his pape , we s udy an
unbounded, s eady, and uni o m shea low ~USF!. While in
molecula luids such a s a e is no possible due o iscous
hea ing, in g anula luids his e ec can be balanced by
dissipa ion in collisions. The simplici y o he model allows
us o ob ain he exac solu ion desc ibing he s eady USF and
also all he physically ele an quan i ies. This is done wi h-
ou in oducing any expansion in he g adien s o in he in-
elas ici y o collisions. The esul s o he p essu e enso
show aniso opy, i.e., no mal s ess di e ences.
I mus be no ed ha ou app oach is qui e di e en om
o he s, in which a speci ic o m is assumed o he one-
pa icle dis ibu ion unc ion desc ibing a gi en s a e. Fo
ins ance, in he heo y by Jenkins and Richman @17#a gen-
e alized Maxwellian is conjec u ed o model he dis ibu ion
unc ion o he s eady USF. The eloci y-independen coe -
icien s a e iden i ied h ough he balance equa ion o he
second o de luc ua ing eloci y co ela ion enso . This
heo y, which in p inciple also keeps all o de s in he shea
a e and dissipa ion, leads o no mal s ess di e ences which
a e in good ag eemen wi h he esul s o molecula dynam-
ics simula ions. On he o he hand, he model we use has
been o mula ed o a bi a y condi ions, and no speci ic ap-
PHYSICAL REVIEW E MARCH 1997VOLUME 55, NUMBER 3
55
1063-651X/97/55~3!/2846~11!/$10.00 2846 © 1997 The Ame ican Physical Socie y
p oxima ion is in oduced o apply i o he s eady USF. To
ob ain he one-pa icle dis ibu ion unc ion one has o sol e
he kine ic model equa ion unde he app op ia e condi ions.
Ano he in e es ing app oach o he same p oblem @18#
has been ca ied ou by expanding he Bol zmann equa ion o
Bu ne o de . The pe u ba i e expansion me hod is speci ic
o he s eady USF, and i is based on he obse a ion ha in
his s a e he shea a e scales as
A
e
, whe e
e
512
a
2. The
heo y esul s in a p edic ion o he no mal s ess di e ences
which a e e y close o hose o Jenkins and Richman, when
he la e a e expanded o he same o de o app oxima ion.
The di ec Mon e Ca lo simula ion me hod @19#was de-
elopped o ob ain nume ical solu ions o he Bol zmann
equa ion, and has been success ully applied o a g ea a ie y
o si ua ions. Since i is o mula ed o an a bi a y sca e ing
law, he e is no di icul y in using i o s udy g anula lows
@20#. He e we p esen esul s ob ained o he s eady USF,
and compa e hem wi h he p edic ions o he model kine ic
equa ion. Fo he componen s o he p essu e enso he
ag eemen u ns ou o be e y good o e a wide ange o
alues o he coe icien o es i u ion. Rega ding he one-
pa icle dis ibu ion unc ion, he ag eemen is only semi-
quan i a i e. This is no su p ising, since he de ailed Bol z-
mann collision ope a o is eplaced in he model by a much
simple e ec i e e m, which is de e mined by he second
momen s o he one-pa icle dis ibu ion.
The s uc u e o he pape is as ollows. In Sec. II he
model is b ie ly discussed, and he basic equa ions a e p e-
sen ed. In addi ion, a u he simpli ica ion o he o mula ion
in Re . @8#in in oduced. I consis s o an e alua ion o he
dissipa ion sou ce e m in he local equilib ium app oxima-
ion. We belie e his is consis en wi h he spi i o he
model, and makes he calcula ions much simple . The model
kine ic equa ion is pa icula ized o he USF in Sec. III, and
he s eady p essu e enso is compu ed in Sec. IV. The esul s
a e compa ed o he heo ies o Jenkins and Richman @17#
and o Sela, Goldhi sch, and Noskowi z @18#. Sec ion V
deals wi h he one-pa icle dis ibu ion unc ion, which is
also compa ed wi h he abo e heo ies in he low dissipa ion
limi . In Sec. VI we discuss he Mon e Ca lo simula ion e-
sul s and, inally, Sec. VII p o ides a sho summa y and
conclusions.
II. BASIC EQUATIONS OF THE MODEL
We conside a gas o iden ical smoo h disks (d52) o
sphe es (d53) o diame e
s
and mass m, whose collisions
a e cha ac e ized by a cons an coe icien o no mal es i u-
ion
a
in he in e al (0,1#. The Bol zmann equa ion o he
one-pa icle dis ibu ion unc ion, ( , , ), is @7,8#
S
]
]
1 1•“1
D
~ 1, 1, !5JB@ 1, 1,
u
~ !#,~1!
whe e JBis he ~inelas ic!Bol zmann collision ope a o
JB@ 1, 1,
u
~ !#5
s
d21
E
d 2
E
d
s
ˆQ~g•
s
ˆ!~g•
s
ˆ!
3@
a
22 ~ 1, 1
8, ! ~ 1, 2
8, !
2 ~ 1, 1, ! ~ 1, 2, !#.~2!
In he abo e exp ession,
s
ˆis he uni ec o poin ing om
he cen e o pa icle 2 o he cen e o pa icle 1 a con ac ,
Qis he Hea iside s ep unc ion, g5 12 2, and
1
85 1211
a
2
a
~g•
s
ˆ!
s
ˆ,~3!
2
85 2111
a
2
a
~g•
s
ˆ!
s
ˆ~4!
a e p ecollisional eloci ies leading a e collision o eloci-
ies 1and 2.
The local pa icle numbe densi y n, low eloci y u, and
empe a u e Ta e de ined in he usual way,
n~ , !5
E
d ~ , , !,~5!
n~ , !u~ , !5
E
d ~ , , !,~6!
d
2n~ , !kBT~ , !5
E
d 1
2m@ 2u~ , !#2 ~ , , !.~7!
F om Eq. ~1! he ollowing e olu ion equa ions o hese
ields a e easily ob ained:
]
n
]
1“•~nu!50, ~8!
]
u
]
1u•“u1~nm!21“•P50, ~9!
d
2nkB
]
T
]
1d
2nkBu•“T52~¹u!:P2“•q2~12
a
2!
,
~10!
whe e
P~ , !5
E
d m~ 2u!~ 2u! ~ , , !~11!
is he p essu e enso ,
q~ , !5
E
d m
2~ 2u!2 ~ , , !~12!
is he hea lux, and
~ , !5m
s
d21
8
E
d 1
E
d 2
E
d
s
ˆQ~g•
s
ˆ!
3~g•
s
ˆ!3 ~ , 1, ! ~ , 2, !~13!
55 2847STEADY UNIFORM SHEAR FLOW IN A LOW DENSITY . . .
is a sou ce e m desc ibing he a e o dissipa ion in colli-
sions.
Sol ing Eq. ~1! o a gi en si ua ion is a o midable ask.
E en in he case o o dina y gases, e y li le is known abou
solu ions o he Bol zmann equa ion o a om equilib ium
s a es, and he p esence o dissipa ion complica es in a non-
i ial way he s uc u e o he Bol zmann equa ion. The sim-
ples physical si ua ion one can hink o o a g anula luid is
he so-called homogeneous cooling s a e ~HCS!, o which
he sys em is uni o m and he ime dependence occu s en-
i ely h ough he empe a u e. Al hough i has been shown
@7,21# ha Eq. ~1!admi s a solu ion desc ibing such s a e, he
exac o m o he dis ibu ion unc ion is no known. Fo
hese easons, i is wo h looking o model kine ic equa ions
simila o hose which ha e p o en o be so ui ul o o -
dina y luids @16#. The basic idea is o eplace he Bol zmann
collision ope a o wi h a simple o m, while p ese ing he
essen ial p ope ies o he exac equa ion.
Ve y ecen ly @8#, a kine ic model along he lines ske ched
abo e has been p oposed. The Bol zmann collision ope a o
is sepa a ed in o wo pa s: one in he eloci y subspace
spanned by 1, , and 2, and he o he one in he subspace
o hogonal o i . The i s con ibu ion is e ained exac ly,
while he second one is app oxima ed by a single elaxa ion
ime e m. This gua an ees ha he balance equa ions ~8!–
~10!a e p ese ed by he model and ha he luxes Pand
q, and also he sou ce e m w, a e he same unc ionals o he
dis ibu ion unc ion as in he Bol zmann equa ion, i.e.,
hey a e gi en by Eqs. ~11!–~13!. Since he de ails a e de-
sc ibed elsewhe e @8,22#, we only gi e he esul he e. The
Bol zmann collision ope a o is eplaced by
JB→2
n
~ 2 l!21
nkBT l
c
~V!~12
a
2!
,~14!
whe e we ha e in oduced he peculia eloci y V5 2u,
c
~ !5m 2
dkBT21, ~15!
and lis he local equilib ium dis ibu ion,
l~ , , !5n~ , !
F
m
2
p
kBT~ , !
G
d/2
exp
F
2mV2~ , !
2kBT~ , !
G
.
~16!
Also,
n
@n( , ),T( , )#is an e ec i e local collision e-
quency, speci ied in mo e de ail below.
The model de ined by Eq. ~14!, al hough much simple
han he o iginal Bol zmann equa ion, is s ill oo complica ed
o allow exac calcula ions in mos o he applica ions. This
is due o he nonlinea unc ional dependence o
on he
dis ibu ion unc ion. Then, we go a s ep u he in he sim-
pli ica ion, and app oxima e
by i s local equilib ium alue,
i.e.,
~ , !→
l~ , !5m
s
d21
8
E
d 1
E
d 2
E
d
s
ˆQ~g•
s
ˆ!
3~g•
s
ˆ!3 l~ , 1, ! l~ , 2, !
5~d21!
S
p
m
D
1/2
n2
s
d21~kBT!3/2.~17!
In summa y, ou model kine ic equa ion is gi en by
S
]
]
1 •“
D
52
n
~ 2 l!21
nkBT l
c
~V!~12
a
2!
l.
~18!
T i ially, his equa ion also leads o he balance equa ions
~8!–~10!, wi h he only di e ence ha in he las o hem he
sou ce e m
is eplaced by
l. In he elas ic collision
limi , he kine ic model educes o he well-known
Bha naga -G oss-K ook ~BGK!equa ion @23#.
Applica ion o Eq. ~18! o he HCS is e y simple. The
solu ion is gi en by a Maxwellian wi h a ime dependen
empe a u e. The ime e olu ion o his la e quan i y is
gi en by Eq. ~10!, which o he HCS has he solu ion
T~ !5T~0!
S
11
0
D
22
,~19!
wi h
0
215~12
a
2!d21
d
s
d21n
S
p
kBT~0!
m
D
1/2
.~20!
As we ha e al eady men ioned, he exac solu ion o he
Bol zmann equa ion o he HCS is no known and, in pa -
icula , i is easy o check ha i is no a Maxwellian ~excep
in he elas ic limi ,
a
51). Ne e heless, bo h heo e ical
s udies @7,21#and Mon e Ca lo simula ions @20#ha e shown
ha de ia ions om Maxwellian a e quan i a i ely small o
he mal eloci ies and Eq. ~19!p o ides a e y accu a e ap-
p oxima ion o he ime e olu ion o he empe a u e.
III. UNIFORM SHEAR FLOW
We wan o s udy he uni o m shea low ~USF!, which is
cha ac e ized by a cons an linea eloci y p o ile
u~ !5a• ,~21!
whe e aij5a
d
ix
d
jy ,abeing he cons an shea a e. Fo
simplici y we conside an unbounded sys em. In addi ion, he
hea lux anishes and he densi y n(0) and empe a u e
T(0) a e uni o m. Fo his low, Eqs. ~8!,~9!, and ~10!imply
ha he densi y is cons an in ime, he p essu e enso is
uni o m, and he empe a u e obeys he ene gy balance
d
2n~0!kB
]
T~0!
]
52aPxy
~0!2~12
a
2!
l
~0!.~22!
.This equa ion clea ly shows he qui e di e en beha io
o elas ic and inelas ic luids unde shea . While o molecu-
la luids he USF is always a ime-dependen s a e whose
empe a u e inc eases mono onically in ime due o iscous
2848 55J. J. BREY, M. J. RUIZ-MONTERO, AND F. MORENO
hea ing, in g anula media he a ia ion o he empe a u e
a ises om he balance o wo opposi e e ec s: iscosi y and
dissipa ion in collisions. As a consequence, a s eady s a e is
possible when bo h e ec s cancel each o he . Ou aim in he
ollowing will be o analyze such a s a e. I is wo h men-
ioning ha shea ed g anula media posses mul iple s eady
s a es, depending on he ini ial and bounda y condi ions @24#.
He e we es ic ou sel es o he USF as desc ibed abo e,
assuming ha he sys em has eached such a s a e, and wi h-
ou paying any a en ion o i s s abili y. A de ailed analysis o
hese ques ions will be published elsewhe e.
Le us in oduce posi ion and eloci ies coo dina es wi h
espec o a ame mo ing wi h he low eloci y u.We
de ine he Lag angian coo dina es by
R5L~ !• ,V5 2a• ,~23!
whe e
Lij~ !5
d
ij2aij .~24!
In e ms o hese, Eq. ~18!becomes
]
]
1LijVj
]
]
Ri
2aijVj
]
]
Vi
52
n
~ 2 l!21
nkBT l
c
~12
a
2!
l.
~25!
Since he USF is mac oscopically homogeneous in he
Lag angian ame, we expec he associa ed dis ibu ion
unc ion, (0), o ha e he same p ope y, i.e., o be indepen-
den o R. The e o e, Eq. ~25! educes o
]
~0!
]
2aijVj
]
~0!
]
Vi
52
n
~0!~ ~0!2 l
~0!!21
n~0!kBT~0! l
~0!
c
~0!
3
~12
a
2!
l
~0!.~26!
This equa ion implies ha
]
^
Vi
&
~0!
]
52a
d
ix
^
Vy
&
~0!,~27!
whe e he angula b acke s deno e a e aging wi h espec o
. The e o e, i he ini ial s a e e i ies
^
V
&
(0)50, his p op-
e y is kep in ime by Eq. ~26!. In he ollowing we will limi
ou conside a ion o ini ial condi ions o his kind. This is he
eason why, o eloci ies in he Lag angian ame, we used
he same symbol as o he peculia eloci ies in oduced in
Sec. II. Then he local equilib ium dis ibu ion appea ing in
Eq. ~26!has he o m
l
~0!~V, !5n~0!
S
m
2
p
kBT~0!~ !
D
d/2
exp
S
2mV2
2kBT~0!~ !
D
,
~28!
wi h all he possible ime dependence occu ing h ough he
empe a u e.
IV. PRESSURE TENSOR
By mul iplying Eq. ~26!by ViVjand in eg a ing o e V,i
is s aigh o wa d o ob ain he e olu ion equa ions o he
componen s o he p essu e enso in he USF,
]
]
Pij
~0!1aikPjk
~0!1ajkPik
~0!52
n
~0!~Pij
~0!2
d
ijp~0!!
22
d
d
ij~12
a
2!
l
~0!,~29!
whe e p5(iPii /d5nkBTis he hyd os a ic p essu e. Fo
a
51 we eco e he equa ions o an o dina y gas unde
USF in he BGK app oxima ion, which ha e been ex en-
si ely s udied @25–27#. F om Eq. ~29!, in pa icula , one ob-
ains
]
]
p~0!52 2
daPxy
~0!22
d~12
a
2!
l
~0!,~30!
]
]
Pxy
~0!52aPyy
~0!2
n
~0!Pxy
~0!,~31!
]
]
Pyy
~0!52
n
~0!~Pyy
~0!2p~0!!22
d~12
a
2!
l
~0!.~32!
This closed sys em o equa ions has he i ial solu ion
Pxy
(0)5Pyy
(0)5p(0)50. A second s eady solu ion, deno ed by
an as e isk, is gi en by
Pxy
*52 a
n
*
F
p*22
d~12
a
2!
l
*
n
*
G
,~33!
Pyy
*52
n
*
aPxy
*,~34!
a2
n
*
F
p*22
d~12
a
2!
l
*
n
*
G
2~12
a
2!
l
*50. ~35!
Fo gi en alues o he shea a e a, he numbe densi y
n, and he es i u ion coe icien
a
, Eq. ~35!de e mines he
alue o he p essu e ~o empe a u e!a which he s eady
s a e is possible. I is con enien a his poin o speci y he
o m o he e ec i e collision equency
n
. Dimensional
analysis equi es ha
n
5cn
s
d21
S
p
kBT
m
D
1/2
,~36!
whe e cis a dimensionless cons an . We a e going o ix his
by equi ing ha he model gi es he co ec ~Bol zmann!
alue o he Na ie -S okes shea iscosi y in he elas ic
limi
a
51. This leads o c516/5b, wi h b.1.016, o
d53~sphe es!, and c52/b, wi h b.1.022, o d52~disks!
@28#. When Eq. ~36!is used in Eqs. ~33!–~35! hey educe o
P
˜
xy52
H
~12
a
2!~d21!
c
F
122~d21!
dc ~12
a
2!
G
J
1/2
,
~37!
55 2849STEADY UNIFORM SHEAR FLOW IN A LOW DENSITY . . .
P
˜
yy52 P
˜
xy
a
˜
5122~d21!
dc ~12
a
2!,~38!
a
˜
25d~d21!~12
a
2!
dc22~d21!~12
a
2!.~39!
We ha e in oduced he dimensionless p essu e enso P
˜
ij
and shea a e a
˜
in he s eady s a e as
P
˜
ij5Pij
*
p*,a
˜
5a
n
*.~40!
Equa ion ~39!shows ha in he s eady s a e he a io o
he shea a e o he collision equency depends only on he
es i u ion coe icien . The simple dependence o he p esu e
enso on he shea a e ound he e con as s wi h he com-
plex one ound in he ime-dependen uni o m shea low o
o dina y gases @25–27#. Le us suppose we ca y ou a se ies
o expe iences, all o hem in he same sys em, i.e., wi h
gi en alues o
a
and n, bu wi h di e en alues o he
shea a e, measu ing he shea iscosi y in he s eady s a e.
Taking in o accoun ha Eq. ~39!implies ha T*}a2,i
ollows om Eq. ~37! ha he gene alized shea iscosi y
h
*is linea in he shea a e,
h
*~a![2Pxy
*
a}a.~41!
O cou se, he p opo ionali y cons an in his exp ession de-
pends on he coe icien o es i u ion.
The o he componen s o he p essu e enso a e easily
compu ed by means o Eq. ~29!, pa icula ized o he s eady
s a e. One ob ains
P
˜
xx5112~d21!2~12
a
2!
dc ,~42!
and, o a h ee-dimensional sys em,
P
˜
zz5P
˜
yy ,P
˜
xz5P
˜
yz50. ~43!
Le us no e ha he educed p essu e enso in he s eady
s a e is exp essed as a unc ion o
a
alone, being indepen-
den , in pa icula , o he applied shea a e. Then, o in-
s ance, o he no mal s ess a ios we ha e
Pxx
*
Pyy
*5dc12~d21!2~12
a
2!
dc22~d21!~12
a
2!,~44!
Pyy
*
Pzz
*51. ~45!
The e o e, he model p edic s aniso opy o he diagonal
e ms o he p essu e enso in he shea plane, bu no in he
plane pe pendicula o he low. The exis ence o no mal
s ess di e ences in shea lows o no mal luids is e y well
known. I is a iscome ic e ec which appea s beyond he
Na ie -S okes app oxima ion @29#. Fo a low densi y USF
hey ha e been calcula ed using he BGK model @27#. The e,
di e ences be ween Pxx and Pyy bu no be ween Pyy and
Pzz we e ound.
As we ha e al eady men ioned, an app oxima ed heo y
o he s eady USF o smoo h inelas ic disks has been o -
mula ed by Jenkins and Richman @17#. Thei esul s o he
second eloci y momen s in he low densi y limi ead, in ou
no a ion,
a
˜
~JR!25~11
a
!~12
a
2!~723
a
!2
c2~917
a
!,~46!
P
˜
xy
~JR!52 4
2529
a
@~917
a
!~12
a
!#1/2,~47!
P
˜
yy
~JR!5917
a
2529
a
,~48!
P
˜
xx
~JR!541225
a
2529
a
.~49!
Al hough hese exp essions may appea a he di e en
om he co esponding esul s ob ained om ou model ki-
ne ic equa ion, Figs. 1 and 2 show ha he disc epancies a e
qui e small o low dissipa ion, and end o anish when
a
app oaches uni y. Le us also men ion ha ecen molecula
dynamics simula ions @24#ha e ound ha he alues o he
s eady empe a u e o a dilu e gas o inelas ic disks can be
closely i ed by an empi ical ela ion, which in ou uni s
eads
a
˜
22516Ac2
p
S
1
12
a
21B
D
,~50!
wi h A.0.080 and B.20.54. The abo e exp ession has he
same unc ional dependence on he es i u ion coe icien as
Eq. ~39!. In addi ion, om his la e equa ion one iden i ies
A.0.100 and B.20.511, which a e su p isingly close o
he simula ion alues, aking in o accoun ha no excluded
olume e ec s a e conside ed in ou model, and also ha he
low obse ed in Re . @24#is highly nonuni o m and i ex-
hibi s ime-dependen mic os uc u es.
Sela, Goldhi sch, and Noskowi z @18#ca ied ou a s udy
o a wo-dimensional g anula USF o Bu ne o de using
he Bol zmann equa ion. They a i ed a exp essions o he
s eady empe a u e and he p essu e enso o he o ms
a
˜
25C~12
a
2!1D~12
a
2!3/21O~12
a
2!2,~51!
P
˜
xy5E~12
a
2!1/21O~12
a
2!3/2,~52!
P
˜
xx511F~12
a
2!1O~12
a
2!2,~53!
P
˜
yy511G~12
a
2!1O~12
a
2!2.~54!
He e C,D,E,F, and Ga e dimensionless cons an s. In
Table I we compa e he alues o hese cons an s gi en in
Re . @18#wi h hose ob ained by expanding he exp essions
de i ed in his sec ion. Also gi en a e he esul s ob ained
om he expansion o he Jenkins and Richman heo y. The
alues om he h ee heo ies a e e y close and, in pa icu-
2850 55J. J. BREY, M. J. RUIZ-MONTERO, AND F. MORENO

la , he ag eemen be ween ou esul s and he Bu ne ex-
pansion o he Bol zmann equa ion is excellen .
V. VELOCITY DISTRIBUTION FUNCTION
The o mal solu ion o Eq. ~26!can be w i en as
~0!~V, !5e2se aijVj
]
]
Vi ~0!~V,0!
1
E
0
d 8e2~s2s8!e~ 2 8!aijVj~
]
/
]
Vi!
F
n
~0!~ 8
!
21
n~0!kBT~0!~ 8
!
c
~0!~V, 8
!~12
a
2!
l
~0!~ 8
!
G
3 l
~0!~V, 8
!,~55!
whe e
s[
E
0
d 8
n
~0!~ 8!~56!
is a measu e o he a e age numbe o collisions pe pa icle
be ween 0 and ,s85s( 8), and exp@ aijVj(
]
/
]
Vi)‡is a shi
ope a o in eloci y space,
e aijVj~
]
/
]
Vi!h~V!5h@L
~2 !•V#.~57!
O cou se, he ime-dependen empe a u e in Eq. ~55!
mus be consis en ly calcula ed, i.e., i is gi en by he solu-
ion o Eqs. ~30!–~32!. Le us now conside he long ime
limi o (0)( ). Assuming ha he s eady s a e discussed in
Sec. IV is eached, we know ha he empe a u e ends o he
cons an alue gi en by Eq. ~39!, and sdi e ges. The con-
clusion is ha (0)(V, ) app oaches he s eady o m
FIG. 1. Reduced shea a e a
˜
as a unc ion o
he coe icien o es i u ion
a
o a wo-
dimensional s eady USF. The solid line co e-
sponds o he p esen heo y, and he dashed line
o ha o Jenkins and Richman.
FIG. 2. The p essu e enso o a wo-
dimensional s eady USF. The solid lines co e-
spond o he p esen heo y, and he dashed ones
o ha o Jenkins and Richman.
55 2851STEADY UNIFORM SHEAR FLOW IN A LOW DENSITY . . .
*~V!5
E
0
`d e2
n
* e aijVj~
]
/
]
Vi!
3
F
n
*21
n~0!kBT*
c
*~V!~12
a
2!
l
*
G
l
*~V!,
~58!
wi h
c
*~V!5mV2
dkBT*21. ~59!
I can be checked ha his exp ession ep oduces he alues
o he s eady p essu e enso ound in Sec. IV, and also ha
i gi es a anishing hea lux. Now we in oduce dimension-
less quan i ies by
V
˜
5
S
2kBT*
m
D
21/2
V,~60!
˜
51
n~0!
S
2kBT*
m
D
d/2
*.~61!
Then Eq. ~58! educes o
˜
~V
˜
!5
p
2d/2
E
0
`dse2sesa
˜
V
˜
y~
]
/
]
V
˜
x!
3
F
12d21
c
S
2
dV
˜
221
D
~12
a
2!
G
e2V
˜
2,~62!
whe e use has been made o Eqs. ~17!and ~36!. In he case
o a sys em o ha d sphe es, he ma ginal dis ibu ion o he
zcomponen o he eloci y is easily ob ained,
˜
z~V
˜
z![
E
2`
`dV
˜
x
E
2`
`dV
˜
y
˜
~V
˜
!5
p
21/2
3
F
122~12
a
2!
3c~2V
˜
z
221!
G
e2V
˜
z
2.~63!
This exp ession shows a limi a ion o ou model kine ic
equa ion, namely, ha he dis ibu ion unc ion akes un-
physical nega i e alues o la ge enough eloci ies. Ne e -
heless, he eloci y alues o which Eq. ~63!is nega i e a e
gi en by
Vz
2.
F
3c
2~12
a
2!11
G
kBT*
m,~64!
and, he e o e, he dis ibu ion unc ion is posi i e in all he
ange o he mal eloci ies, e en in he limi
a
→0. I is hen
possible ha Eq. ~62!p o ides an accu a e app oxima ion o
he solu ion o he Bol zmann equa ion in all he ele an
egion o he dis ibu ion unc ion. This poin will be ana-
lyzed in de ail in Sec. VI.
The ma ginal eloci y dis ibu ion in he shea plane, also
o d53, is
˜
xy~V
˜
x,V
˜
y![
E
2`
`dV
˜
z
˜
~V
˜
!
5
p
21
E
0
`dse2se2[~V
˜
x1sa
˜
V
˜
y
!
2
1V
˜
y
2
]
3
H
12
4
~
12
a
2
!
3c@~V
˜
x1sa
˜
V
˜
y!21V
˜
y
2#
J
.
~65!
In o de o compa e wi h p e ious heo ies, we ha e ca ied
ou a pe u ba i e expansion o
˜
o d52 in powe s o
12
a
2. The esul is
˜
~V
˜
!5
p
21e2V
˜
2
F
12V
˜
2sin2
u
A
c~12
a
2!1/2
1~122V
˜
21V
˜
2cos2
u
11
2V
˜
421
2V
˜
4cos4
u
!
312
a
2
c1O~12
a
2!3/2
G
,~66!
He e, we ha e in oduced a pola ep esen a ion o he e-
loci y, V
˜
(V
˜
,
u
), whe e
u
is measu ed wi h espec o he
s eaming di ec ion x.
Jenkins and Richman @17#assumed ha he s eady dis i-
bu ion unc ion has he o m o a gene alized Gaussian,
˜
~JR!51
p
A
u
K
u
exp~2V
˜
•K21•V
˜
!,~67!
whe e Kis a ma ix which accoun s o he aniso opy exis -
ing in he USF. When he low densi y limi o he abo e
dis ibu ion is conside ed and he esul expanded o o de
(12
a
2) one ob ains
˜
~JR!~V
˜
!5
p
21e2V
˜
2
F
12V
˜
2sin2
u
A
2~12
a
2!1/2
1~122V
˜
212V
˜
2cos2
u
11
2V
˜
421
2V
˜
4cos4
u
!
312
a
2
41O~12
a
2!3/2
G
.~68!
I we neglec he di e ence be ween c(;1.96) and 2, bo h
exp essions ag ee o o de (12
a
2)1/2. The e ms o o de
(12
a
2) ha e he same dependence on he eloci y modulus
TABLE I. Compa ison o he alues o he coe icien s in ex-
pansions gi en by Eqs. ~51!–~54!ob ained wi h di e en heo ies
and in he p esen wo k.
Model Sela, Goldhi sch,
and Noskowi z Jenkins and Richman
C0.511 0.511 0.522
D00 0
E20.714 20.714 20.707
F0.511 0.522 0.5
G0.511 0.522 0.5
2852 55
J. J. BREY, M. J. RUIZ-MONTERO, AND F. MORENO
and also on
u
, bu all he cons an p e ac o s di e . In spi e
o his di e ence, le us no ice ha bo h exp essions ~66!and
~68!make he same con ibu ion o he diagonal pa o he
p essu e enso when he cons an cis again app oxima ed by
2. This can be e i ied by a di ec calcula ion ~see also Table
I!.The dis ibu ion unc ion o he USF o a wo-
dimensional g anula gas has also been calcula ed a he
same o de by Sela, Goldhi sch, and Noskowi z in Re . @18#.
The e, a much mo e complica ed dependence on bo h pola
componen s o he eloci y is ound. By compa ing wi h Jen-
kins and Richman esul s, he au ho s conclude ha he con-
s an s appea ing as p e ac o s o he second ha monics in
u
in Eq. ~68!can be conside ed as ough a e ages o he
co esponding unc ions ob ained by hem. We e e he
eade o hei pape o de ails.
VI. DIRECT MONTE CARLO SIMULATION
The di ec simula ion Mon e Ca lo me hod @19#has
p o ed o be a e y use ul ool o ob ain nume ical solu ions
o he Bol zmann equa ion o molecula luids. Ve y e-
cen ly, i has also been applied o s udy he HCS o a low
densi y g anula low @20#. Since he de ails o he me hod
ha e been ex ensi ely discussed in Re . @19#, hey will no be
gi en he e.
We saw in Sec. III ha he dis ibu ion unc ion o he
USF becomes homogeneous in he Lag angian ame. The
conside a ion o homogeneous s a es allows a g ea simpli i-
ca ion o he simula ion. The e o e, we ha e ca ied ou he
simula ion in he Lag angian ame and es ic ed ou sel es
o solu ions o he Bol zmann equa ion which s ay homoge-
neous in ha ame. In o he wo ds, we nume ically sol ed
he equa ion @compa e wi h Eq. ~26!#
]
~0!
]
2aijVj
]
~0!
]
Vi
5J
B@V
u
~0!#.~69!
O cou se, his implies ha he possibili y o spon aneous
o ma ion o spa ial inhomogenei ies is elimina ed in he
FIG. 3. Time e olu ion o he educed shea
a e a
¯
o
a
50.8, and di e en alues o he
shea a e a. In all cases, he ini ial dis ibu ion
was homogeneous wi h a Maxwellian eloci y
dis ibu ion in he Lag angian ame. Time is
measu ed in uni s o c„2
A
pn
(0)…21.
FIG. 4. S eady educed shea a e a
˜
as a unc-
ion o he coe icien o es i u ion
a
o a dilu e
sys em o ha d disks. The solid line co esponds
o he kine ic model, and he symbols a e esul s
om he Mon e Ca lo simula ion.
55 2853STEADY UNIFORM SHEAR FLOW IN A LOW DENSITY . . .
simula ion. Ou aim he e is o s udy he p ope ies o he
homogeneous s eady s a e. I s s abili y will be analyzed else-
whe e.
Fo homogeneous sys ems he e is no need o spli he
sys em in o cells and, consequen ly, he spa ial coo dina es
o he pa icles do no play any ole in he simula ion. In
addi ion, no bounda y condi ions mus be in oduced. In ou
simula ion we ha e conside ed a h ee-dimensional sys em.
The numbe o pa icles is N51000, and he esul s ha e
been a e aged o e 500 di e en ajec o ies. The ime in e -
al D o e which i is assumed ha ee mo ion, including
he e ec o he ine ial o ce, and collisions, a e uncoupled
has been aken
d
50.025
n
0
21, whe e
n
05(2
A
p
/c)
n
( ),
wi h
n
( ) being he ins an aneous alue o he collision e-
quency gi en by Eq. ~36!. We conside ed a noncons an ime
s ep in o de o gua an ee ha i always emains much
smalle han he a e age ime be ween collisions, in spi e o
he change o he empe a u e @30#. The ini ial eloci y dis-
ibu ion in all cases is a Maxwellian.
In Fig. 3 we p esen he ime e olu ion o a
¯
[a/
n
( ) o
a
50.8 and ou di e en alues o he shea a e, namely,
a50.1, 0.25, 0.5, and 1. Time is measu ed in uni s o
c„2
A
pn
(0)…21, whe e
n
(0) is he ini ial collision e-
quency. A e an ini ial ansien pe iod, all cu es con e ge
o he same s eady alue, as p edic ed by Eq. ~39!. The same
quali a i e beha io has been ound o all he educed com-
ponen s o he p essu e enso Pij( )/p( ). The e o e, in he
ollowing we will concen a e on he dependence o he
s eady alues o he educed quan i ies on he es i u ion co-
e icien
a
, once we ha e checked hey do no depend on he
shea a e.
The esul s ob ained o he s eady educed shea a e a
˜
o di e en alues o
a
a e shown in Fig. 4. The s a is ical
e o s a e smalle han he symbols used o ep esen he
da a. Also plo ed is he p edic ion o ou model kine ic
equa ion, i.e. Eq. ~39!wi h d53. I is seen ha he ag ee-
men is ema kable a low dissipa ion, al hough he disc ep-
ancy inc eases as he es i u ion coe icien dec eases. We
FIG. 5. The same as in Fig. 4 o he educed
p essu e enso P
˜
ij.
FIG. 6. Ma ginal eloci y dis ibu ion unc-
ion in he di ec ion pe pendicula o he shea
plane. The symbols a e simula ion da a, and he
solid line co esponds o he model kine ic equa-
ion. The es i u ion coe icien is
a
50.8.
2854 55
J. J. BREY, M. J. RUIZ-MONTERO, AND F. MORENO