Internat. J. Math. & Math. Sci.
VOL. 13 NO. (1990) 93-114
93
HODOGRAPHIC STUDY OF NON-NEWTONIAN MHD ALIGNED STEADY PLANE FLUID FLOWS
P.V. NGUYENandO.P.CHANDNA
Deprtm,’nt
of Mathematics and Statistics University ofWindsorWinds,,r,Ontario N9B 3P4,Canada (Received May 22, 1989)
ABSTRACT. A study is made of non-Newtonian HHD aligned steady plane fluid flows to find exact solutions for various flow configurations. The equations of motion have been transformed to the hodograph plane. A Legendre-transform function is used to recast the equations Jn the hodograph plane in terms of this transform function. Solutions for various flow configurations are obtained. Applications are investigated for the fluids of finite and infinite electrical conductivity
bringing out the similarities and contrasts in the solutions of these types of fluids.
KEY WORDS AND PHRASES. Steady, Non-Newtonian Magnetofluid dynamic, incompressible, plane, Hodographic study, Aligned.
1980 AMS SUBJECT CLASSIFICATION CODE. 76W05.
1.
INTRODUCTION.
Transformation techniquesareoftenemplo:y-dforsolvingnon-linearpar- tialdifferential equations andhodographtransformalionmethodisoneof these techniqueswhich has been widely used in continuummechanics. W. F. Aes[1]
has given an excellentsurveyof thismethodtogetherwith its applicationsin variousother fields. This paper deals with tle ap- plication ofthismethodfor solvingasystemof non-linear partialdifferentialequations governing steadyplaneincompressible flow ofanelectrical conducting second-gradefluid in thepresonceofanalignedmagneticfield. Recently, A. M. Siddiquiet al
[2]
usedthe hodograph and Legcndre transformationstostudynon-Newtoniansteady planefluid flows.O. P.
Clandnaet al[3]
hasalsoappliedthistechniquetoNavier-Stokes equations. Since electrical conductivityisfinite for most liquid metals andit is also finite forother electrically conducting second gradefluids to which singlefluidmodelcan be applied,ouraccounting for thefinite electrical conductivity makesthe flowproblemrealisticand attractivefrom bothaphysicalandamathematical point ofview. We havealso included electricallyconductingsecondgradefluids ofinfinite electrical coaductivityto makeathorough hodographic studyofthesefluidflows and torecognize the dawnan,tfuture of superconductivityin science.
Westudyourflowswiththe objective ofobtainingexactsolutions tovariousflowconfigura- tions. Westart withreducingthe order of governing equationsby employing M. l:I. Mtrtin’s
[4]
perceptiveideaof introducing vorticity and energy functions. Theplanofthispaperisasfollows:
In
section 2the equations arecast intoa convenientform for this work. Section 3 contains the transformationof equationstothe hodograph planesothat the role of independentvariables:.y and thedependentvariablesu,v(the
twocomponentsof the velocity vectorfield)
isinterchanged.Weintroducea Legendre-transformfunctionof the streamfunctionand recast all ourequations inthehodograph planeintermsofthistransformfunction inSection4. Theoreticaldevelopment
94 P.V. NGUYEN AND O.P. CHANDNA
ofsection4 isillustratedbysolutions to thefollowingexamples in section 5:
(a)
flowswithelliptic and circular streamlines(b)
hyperbolic flows(c)
spiral flows(d)
radialflows.These applications are investigated for the fluids of finite and infinite electrical condlctivity bringingoutthe sinfilarity and contrastsin thesoluti,ns of these two types offlfids.
2.
EQUATIONS
OF MOTION. The steady, planeflow ofaninconpressible second-grad’flid of finite electricalconductivityisgoverned bythefollowingsystem of equations:Ou + -
Oyo
oo 0,,)
0-+v N +N
OHx. OH2
Oz +--y
=0where u,varethecomponentsof velocityfield ]7
, H, H2
the components of the magm.ticvector field]E?,
andp isthe pressurefunction: allbeingfunctions of x,y.In
this systemand c2 arerespectively the constant fluid density,the constant coefficient of viscosity, thecon-
HODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS 95
stant magnetic permeability, theconstant electrical conductivity and the normal stress moduli.
Furthermore,
K
isanarbitrary constant of integration obtained from thediffusionequationWe
nowintroduce the twodimensional vorticityfunction w, the current densityfunction j and energyfunctione definedbyOv Ou OH2
where
q2
Ial
intothe above system of equations d obtn thefoong system:
+ Ov
0 (otity)o V ax vV2w
*jH(Bne momentm)
ug vg
j1+
g(ffusion)
OHa
OH,_0--- +
0(solenoidal)
OH: OHa
(current
density)w
(vorticity)
0 0v
(2)
ofseven partial differential equationsin sevenunknown functions u,v, w,
Ha,
H2, j and e as functionsof z,y. This system governs the motionofsecond-gradefluidoffinite electrical con- ductivity.For
themotionofsecond-gradefluid of infinite electrical conductivity,weonly replace thediffusionequationintheabove systembyuH2
vHi
K.ALIGNED FLOW.
A
flowissaidto beanalignedorparallelflow if the velocity and the magnetic fields areeverywhere parallel. Takingour flow to bean aligned flow, there exists some scalar functionf(z,y),
called theproportionality function,such thatit f(,v)V (3)
Introducingthisdefinition of the magnetic vector fieldintheabovesystem,thealignedflow isgoverned bythefollowingsystemofsevenequations
+
_x-- 0(4)
Oe O
pvw I--a--
a,vV2w
I*fvj(5)
96 P.V. NGUYEN AND O.P. CHANDNA
#,oj+K=0
1(7)
" of Of +’N Of
=0(s)
f + i
=w
(10)
Oz
i i,,k-ofu-tio-
,,(:, ), ,,(:, ),,,,(:, ), f(, ),./(:, u), (:, )
,d=
bit,-yo.t,tK. Once
a solutionof this system isdetermined, the pressure and the magnetic functions are obtainedbyusing the definition ofein(1)
and the definition of in(3)
respectively.3.
EQUATIONS
INTHE HODOGRAPH PLANE.
Letting the flowvariablesu(z,y),v(z,y)
be suchthat,inthe region offlow,theJacobian0(.,) g(’Y)
o(:y) # o, o < IJI < ()
wemay considerx and yasfunctionsofuandv.
By
meansofz:r(u,v),y
y(u,v),wederive thefollowingrelationsOu Oy Ou
o-
o%J-- Or’ Oy -= Ov Ov Oz I (12)
and
Og O(g, z) =O(:) (13)
h.
a a(,) a((., ), (,)) (.,)i
.y oti.uo]y aifftiUtion ndJ J(’/=
0(,/- [0(,/l J(’/" (4/
Emplonghese transformation relations fortge flrs order partiderivatieesappearingi systemof
euations (4) (10)
and thetransformationequations for thefunctions,j,],
edefined by.(,) ((=,),(=,)) z(=,), j(,) j((,),(,))
j(,),f(x,y) f((u,v),y(u,v)) f(u,v),
(,) ((,),(,)) (,),
thesystem
(4)-(10)
istransformedintothefollowing systemofsevenequationsinthe(u,
v)-ple:-0(, [o(, o(,
x,
)
+ + ,"
fuj(17)
,.) - +.gw + ’] t(’Jw’) o(w,)
HODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS 97
where
p.--j + K
0(18)
o(f ,) o(,f)
uO(u,v) + O(u,v)
0(19)
-[ o(7,,) o(,,7)]
I + s ,,,,) "o(,,,,)j s (uo)
J 0v "- (21)
0(,=)
/
w =w(,)- 0(,) (2)
0(,v)
for the sixunknown functions, z, y, w, e,
,
ofu,v andan arbitrary constantK
when, W, Wu
areenated, using(14)
and(22).
Once a solution x
x(u,v),
y y(u,v),(u,v), (u,v),
j j(u,v),f f(u,v)
isdeterned, we are led to thesolutionofuu(x,y),
v v(x,y) and thereforew(u(x,y),v(z,y)) w(x,y),
ee(x,y),
j j(x,y),f
](x,y) for the system(4) (10)
governingthefitely conductingflow.The aboveanMysis
Mso
holdstrue forinfinitely conductingsecond-grade
fl,fidflows. How- ever,for theseflows,the arbitrary constantK
0 and equation(7)
anditstransformed equation(18)
are identicMlysatisfied.4.
EQUATIONS FOR THE
LEGENDRETRANSFORM FUNCTION
ANDF(U, V).
Theequa- tionof continty impfies theestence
ofastreaunction(x,y) such thatd=-vdx+udy or =-v, =u.
(23)
Likewise,
(15)
impliestheexistenceofafunctionL(u, v),
called theLegendre
transformfunction of thestreamfunction(z,y),
sothatOL OL
dL=-ydu+zdv or
0u =-Y’ 0v =x
(24)
and the twofunctions
(z,y), L(u, v)
are related by(25)
IntroducingL(u,v)
intothe system(15)-(21),
withJ,
W1,W
givenby(14), (22)
respec- tively,itfollows that(15)
isidenticallysatisfiedandthissystemmaybereplaced by-o s ( w. ) o(o,sW‘)
o-..,
’0.sw ,,.s O(u,v)
--,o, , o(r,Tw,)
-o-(V..; -,,..o,+ .sw. + ....s
O(u,v)
(,-w,)
00L (,7) o(OL
+ ’7) o 19.9
o(,,,,,) o(,,,,,)
(28)
98 P.V. NGUYEN AND O.P. CHANDNA
wherenow
(30)
(31)
J Ov \ (32)
w, O(u,v)
W_=O(u,v) (33)
for thefive functions
L(u,v), (u,v), E(u,v),
j(u,v),f(u,v)
andan arbitraryconstantK,
afterJ, Wz, W2
areelinfinated.By
using theintegrabilitycondition OL 0OuOv
0%i.e.
oro---
2eo,o---=t
in(z,
y)-plane,weeliminate(u, v)
from(26)
and(27)
andobtain-[ O(
or,j-)
+ t,*f ,,
O(u,,) +" 0(,,,,,) j
(34)
(a)
Since j has a constant value-#*oK
forafinitely conductingfluidas givenby(28),
it follows thatL(u,v), f(u, v)
satisfyequations(29), (30)
andv(,,- + ,,w).
(35)
(b)
Equation(28)
isidenticallysatisfiedforaninfinitely conducting fluid flow_and
j isgivenby
(30).
Elirninating from(30)
and(34),
wenna
thato
thenows L(,,v)la/(=,)
satisfy equations(29)
andHODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS 99
o(, ,) o,
o( 7{o( -w,)/o,,,+o(
L7w)/oo, }) + a
v(u, v) +u O(L’ 7{0( ffW)
/O(u’v)+O(O(u,v) , 7W:) /O(u v)})]
J(36)
+ .]
0o o
where
F
andF
are definedO( o(
(’ 0(, 0(,
Suingup,wehave thefoowingtheorems for finitely conductingandinfitelyconducting
TgeoN
I.
If(, v)
is le Legendre lrsfom function ofa streunction ofseady ple gnedo
of incompressibleecond-grede
d ofte
ecricMconductivity df(, v)
iste
lrsformed proporlionty function,le(, v)
dI(, v)
mlsatisfy equations(29), (0)
d() ere
j(,v),{,v), J(,v), W(,v), W(,v)
een b
equations(28), () o ().
Teoe
II. (, v)
ileLegendrelrsform fnction ofareunction ofte
eque- lionsgoerMng leed
plegned o
ofincompressiNesecond-ade
dofinteelecN-cM
conductity df(u, v)
isthetrsformed proportionty function, thenL(u, v)
df(u, v)
mustsatisfyequations
(29)
d(36)
where(u,v), (u,v), ff(u,v), W(u,v), W(u,v), F(u,v), F(, ) Once
a.
sdutiony (30) L
toL(u,v),f (33) a (3Z). 1(u,v)
isfound, for wh’chJ
evuatedkom(32)
satisfy0
< IJI < ,
the solutionsfor thevdocitycomponentse obtMnedbysdngequations(24)
simteously. Having obtMned the vdocity componentsu
u(z,y),
v v(x,y), weobtMnf(x,y)
in thephysicMpleom
the sdution forf(u,v)
in thehodograph
ple.We,
then, obtMn the vorticity, the current density d theener
functionsbyusingV(z,y)
df(z,y)
in equations(10), (9), (5)
d(6).
FinMly, the pressurefunctiond the magneticvector fi’cldaredeterned
om (1)
d(3).
Asvariousassumed forms forLegendretransformfimctionarebest handledifpolarcoordi- natesinthehodograph planeareemployed,wenowdevelopthe results of the above theoremsin polarcoordinates (q,
0)
inthe hodograph plane. Expressingu
+
iv qei#, (38)
wehave the followingtransformations:
100 P.V. NGUYEN AND O.P. CHANDNA
0 0 sin 0 0 0 0 cos0 0
=cosOoq
q00’
o%--=sinOb// +
q O00( F, G) 0(F*, G"
0(q,0 10( F’,
G*O(u,v) O(q,O) "O(u,v)
qO(q,O) (39)
where
F(u,v)=
F(q,O),G(u,v) G*(q,O)
are continuo.sly differentiablefunctions. On using theserelations,and regarding (q,O)
as newindependentvariables, the expressions for J,, Wa.
W,Fa, F
and j inthe (q,O)
plane,take the formsj.(q,O)=q4 [q202L* -0
2(OL* q+ OL ") (OL* 3-qb 02L’)2] -’ (40)
[OL 10:L
IOL*w’(q,O)
=S"[+ q,
00+ j (41)
W;(q,) 0 (
sin+o,
q
O(q,) (42)
W;(q,) (43)
q
(44) F;(q,)
0
o
oz"I"
q
O(q,)
F;(q,O)=-IO
sinO+ o,(45)
q O(q,
O)
0
0 cosO
"
,i=oz"/.
j*(q,O)=f*w’+J* sin
(
0i
oo’)
o(,o
cos0
0(q, 0)
j’(q,O)
-’eK
iaen
in(46)
ifthefluid isflnitel
conducting. Equations(29), (aS)
and(a6)
aretransformedto the(q,O)-plane
0 L*
Of"
0 L"Of"
10L"Of"
-
=0(47)
Oq
O0OqO0
0q qO00q
(48)
HODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS i01
(49)
where
X*
isdefinedas(50)
Having developedthe abovetransformations,westate thefollowingcorollaries which respec- tively follow fromtheorem andII:
COROLLARY I.
/fL*(q, O)
andf*(q,O)
istheLegendretransformfunctionofastreamfunction and the proportionalityfunctionrespectively ofthe equationsgoverning themotion ofsteadyplane alignedflow ofanincompresslblesecond-gradefluidof tinite electricM conductivity, thenL*(q,0)
and
f*(q,O)
mustsatisfy equations(46), (47)
and(48)
whereJ*(q,O), o*(q,0),
W(q,O), W(q,O) andx*(q, O)
aregiven by(40)
to(43)
and(50).
COROLLARY" II.
lfL*(q,O)
andf*(q,O) aretheLegendretransform ofastreamfimctionand the proportionalityfunctionof the equations governing themotionof steadyplane alignedflow of anincompressible second-gradefluid ofin/niteelectrical conductivity, thenL’(q,O)
andf’(q,O)
must satisfy equations(47)
and(49)
whereJ*(q,O), w*(q,O), W(q,O), W(q,O), F(q,O), F(q,O)
andx*(q,O)
aregivenby(40)
to(45)
and(50).
Once
asolutionL*(q,O), f*(q,0)
isobtained,weemploytherelationsOL* cos00L* sin00L* OL*
z sinO
_---- +
y+
cosO--(51)
q O0 q O0
Oq
oq
and
(38)
to obtain the velocity components u u(z,y), v v(z,y) in the physical plane.Followingthedeterminationof velocitycomponentsu
+
iv qei inphysical planewegetf(z, V)
and the other remaining flowvariables.I02 P.V. NGUYEN AND O.P. CHANDNA
5. APPLICATIONS. In thissectionweinvestigatevariousproblemsas apI)licationsofTl,’(,rem and
II,
and theircorollaries.APPLICATION
I. LetL(u,v)
Au+
Bv+
Cu+
Dv+ E (52)
be the Legendretransformfunctionsuch that
A, B, C, D, E
arearbitrary constants and A,B
are nonzero. Using(52)in
equations(31)
to(33),
weget1
A+B
Wa
=0,W2=0. (53)
J= 4AB 2AB
Wenowconsider finitelyconductingand infinitely conductingcasesseparately by applying theorem and theorem
II
respectively.FINITELYCONDUCTINGFLUID.
EIiminatingL(u,v),(u,v), J(u,v), Wa(u,v), W2(u,v)
and j(u,v) from equations(29), (30), (35)
byusing the expressions for these functions from(52), (53)
and(28),
wefind that equation(35)is
identicallysatisfied and f(u,v)
must satisfyAuOf
Bv =0cO] cO-] (54)
(A + B)f + av-v + Bu-- + 2ABK,*o
0if
L(u,v)
given by(52)
is the Legendre transform function ofa streamfunction offinitely con-ductingfluid flow.
Solvingequations
(54),
wehave, (,, + .)-.-5 (.)_
a.K,’.;
-f(u, v)
AKin" atn(u +
v:) + (u)
where arbitraryfunctions
(u)
and(u)
mustsatisfyA - -B } (55)
A=-B
and
{B’(u)}v + {B’(u)u + -(A
1 :zB2)u(u)}
0{’(u)}v + {4AK*au}v + {u’(u)}
0(56)
Since equations
(56)
and(57)
hold true for everyv, andA #
0,B #
0,it follows that wehave thefollowingthree possiblecases:
(i) L(u,v) A(u + v:) + cu +
Dv+ E, -](u,v)
C,(u+ v’)
-*AKI’a
whenA B #
0 andCis an arbitrary constant.(ii) L(u v) Au
2+ Bv +
Cu+
Dv+ E, -](u v)
-2AB_,’,,A+BwhenA#0, B:/=0
andA #
+B.(iii) L(u,v)=A(u 2-v 2)+cu+ov+E, f(u,v)=C2
whenA=-B#0, C2
isanarbitraryconstantand
K
0.Wenow proceedtostudy thesethreecasesseparately.
CASE
(I).
UsingL(u, v) A(u +
v2) +
Cu+ Dv + E
in(24)
and solving the resulting equations simultaneously,wegetEmploying(58)in
f(u,v) Ca(u
2+ v2) - AKIn*a,
weobtain(57)
HODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS 103
f(z,y)
4C1A [(y + C) + (, D)2)]
-1AK#’a.
Substitutingfor
u(z,y),v(z,y)
andf(z,y)
inequation(3),
wehave]q(z,y) {4CxA2[(y + .( y+C
2Az-D) C)’
2A+ (z D):] - AK#’a}
(59)
Usingw
X’
e(z,y). Usingthis solutionfor
e(z,y)
and(58)in (1),
thepressure function isfound to be p(zy) (
8A:PK2#’3a2
4) [(Y + c)2 + (z
+ K#"aC:
Agn[(y + C)’ + (z 9) + C3
where
C3
isanarbitrary constant.(60)
j
-K#’o,
equations(58), (59)
in(5), (6)
and integrating, wedeternfine(61)
CASE
(II). In
this case, wehaveL(u,v) Au + Bv +
Cu+ Dv + E,
and
A #
-I-B. Proceedingasin case(i),
weobtainf{u ,)=
-AOU.’,,A+B2A 2B
where
C4
isan arbitrary constant.CASE (III). In
this case,L(u,v) A(u
v) + Cu + Dv + E
and-](u,v) C2.
Flowvariables forthiscaseare:2A 2A
i7 c=V
P
[(y+C) 2+(z-D) 2] +
p(=,)
C
where
C5
isanarbitrary constant.3ax + 2a2 (63)
INFINITELY CONDUCTING FLUID.
Using theexpressions forL, J, , W,
W2,F, F2
asgivenby
(52), (53), (37)
inequations(29)
and(36),
wefindthatst(u, v)
must satisfyo.t oI
Au-- Bv--
0of o!
v
N - =o (64)
Solving equations
(64)
forf(u, v),
wefindthatf(u, v) (u +v 2)
ifA
Bandf(u, v) C
if
A : B,
where is an arbitrary function ofits argument andC6
is an arbitrary constant.Therefore,wehave the followingtwocases:
104 P.V. NGUYEN AND O.P. CHANDNA
(i) L(u, v) A(u
2+
v) + Cu + Dv + B, "(u, v) q(u + v),
where isanarbitraryfunction ofitsargument.
(ii) L(u,v) Au
:+
By+Cu+Dv+E,,’-/(u,v) C6
whereC6
isanarbitraryconstantandB
#A.
We
now consider these twocasesseparately.
CASE
(I).
Without loss ofgenerality, wetake j(u,v) u+
v.
UsingL(u,v) A(u +
v2) +
Cu
+
Dv+ E
inequations(24),
weobtain-i=(u,v)= ( Y+C2A’z-D)2A (65)
andtherefore.
,((x,y)
1-- [(y + C) + (x D)]. (66)
Employing
(65)
and(66)in (9),
weobtain j(z,y) 1A [(u + C) + (z D)].
(67)Using
(65)
to(67)
inequationsinthephysicalplane,weobtain[(Y+C)+(z-D)] y+C 2A’
z2AD
(68)
(,) (
P’)
where
Cv
is arbitryconstant.CASE
(II).
UsingL(u, v) Au +
By+
Cu+ Dv + E
whereA B,
and(u, v) C,
weobtnV=(u,v)= ( Y+C2A ’x-D)2B
j(z,y)
A+B 2AB..Un
3aa +
(,U)= [(u+C)’+(’-D)’]+
8AB
(69)
8A:Bwhere
Ca
is arbitraryconstant.Suingup,wehave thefollowingtheorems:
TnEoaE III. H L(u,v) Au + Bv + Cu + Dv + E
is theLegene
trsform ofastreunctionforasteady, ple, gned
o
of incompressiblesecond-grade dof nite ectricMconductity, then theow
in the physicMple(a)
avortexo ven
byequations(58)
to(51)
whenA B
inL(u, v).
(b)
ao
withhyperbocstrenes
witho
viablesgivenby(63)
whenB -A
in
L(u, v).
when
B #
iA.TnEORE
IV. H L(u,v) Au + Bv + Cu +
Dv+ E
is the Legcndre transform ofastrenfunctlon for a steady, ple, Migned, incompressible innitely conducting second-grade uid
o,
then theo
in the physicMpleis:HODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS 105
(a) (b)
a vortexflowwith flowvariablesgiven by
(65)-(68)
whenA B
in L(u,v).aflow withflowvariablesgivenbyequations
(69)
with thestreangincswhenB A
inL(u,v).
APPLICATION II" Welet
L(u,v) (Au + B)v +
Cu+
Du+
E (70)to be the Legendre transform function, where
A,B,C,D,E
are arbitrary constants andA
isnollzero.
Evaluating
J, , W1
and W2, byusing(70)
inequations(31)
to(33),
wegetJ=
2CA:’
W-A:’ W, =W
=0.(71)
FINITELY CONDUCTING
FLUID.
Using equations(28), (70), (71)
in equations(29), (30), (35),
wefindthatequation(35)
isidenticallysatisfiedandf(u,v)
mustsatisfy equations(2Cu + Av)- Au--
0(72)
Of Of A K
2C
I -t-(2Cv A
u-v A
V-u
Multiplying
(72)
byv,(73)
byuandsubtracting,weobtain(73)
Of
2Cu u-- A(u: + v)f + AK#’au + v
0(74)
Solvingequations
(72)
and(74),
wegetA
](u v)= exp[-tan-’ ;](u)+n
a,C0
-AK*at-’ () + (u), C
0where arbitrary functions
(u)
and1/,(u)
must satisfy[Au’(u)]v -[4Cu(u)]v + [Aua’(u) 4C -X- (,,)] o,
c#o
(75)
and
[u’(u)lv + [2AKp oulv + [u’(u)l
O,C=O.
(76)
Equations
(75)
and(76)
hold true for all v if(u)
0 and/,(v)
D, where D, is anarbitrary constant. Therefore,wehave the followingtwo cases:
(i) L(u,v) (Au + B)v +
Cu+
Du+ E, f(u,v) K.’o,
when C 0.(ii) L(u,v)=(Au+B)v+Du+E,f(u,v)=Dx-
Using
L(u,v)
and](u,v)
for the two cases and proceeding as in application I, the flow variablesin thephysicM planeareobtained to be:I06 P.V. NGUYEN AND O.P. CHANDNA
CASE
(I).
V (u’v) (
z,2CB- AD-
2Cz-] A K
2Cl a-
P
[(x B): +
(y+ D) 2]
2A
gl
.3a[Ay(x-B)+C(x-B) :+ADz,]
2C
A +C + (6al + 4a2)
A4
+ D
where
D2
isan arbitrary constant.(77)
CASE (II).
u’v
(
z y+ D
p
6al + 4a2
V(x,V) D3 [(z B) +
(y+ D) ] +
A2(78)
where
Da
isan arbitrary constant.INFINITELY
CONDUCTING FLUID.
UsingL, , , Wa,
W2,Fx, F2
#yenby(70), (71), (37)
in equations
(29)
d(36),
wefind thatl(u, v)
must satisfy(ff + v)
0Solving
(80),
weobtain(u,v) D4 (80)
where
D4
isan arbitraryconstant.We employ
L(u,v), f(u,v)
givenby(70), (80)
respectivelyin(24), (3)
and equationsin the physicalplane,and obtain(u’v) (
z,2CB- AD-
2Cxand
p(z,y)=DL- -i[(z-B +(y+D
2nl*C
C(x
B)A:
y(zB) + + Dx (81)
A +C
+ (6Ctl + 4Ct2)
A4where
D5
isan arbitrary constant.Summingup,wehave thefollowingtheorems:
THEOREM V. /f
L(u,v) (Au + B)v + Cu +
Du+ E
istheLegendre transform fimction ofastreamfunctionforasteady, plane, ah’gned, incompressible,tlnitelyconducting second--grade fluidflow,then the flowin the physicMplaneisHODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS 107
() (b)
given byequations
(77)
havingCx+ Axy ABy +
(AD2BC)z
constantasitsstreamlines whenC 0 in L(u,
v).
a flowwih recangd hyperbol
(z
B)(y+ D)
constan itsstreamlines d isgiven byequations(78)
whenC 0inL(u, v).
THEOREM VI.
HL(u,v) A(u + B)v+Cu +
Du+ E
istheLegendre transformfinction of astreamfunction ofasteady, plane, ah’gned, inconpressible, intinitelyconducting second-grade fluidflow,then the flowin the physicalplaneisgivenbyequations(81)
withCz
+ Azy- ABy + (AD 2BC)z
constantasitsstreamlines.
APPLICATION III: Let
L*(q,O)
F(q); F’(q) O, F"(q) #
O.(82)
Using
(83)
in(40)
to(43)
and(51)
toevaluateJ*, w*,W*, W,
z and y, wegetj. q
,.
aF"(q)+
F’(q)F’(q)F"(q)’
F’(q)F’(q)W lw" cosOF’(q), W; -w" sin0F’(q),
q q
x
F’(q)sin e,
y=-F’(q)cosO (83)
Wenowstudyfinitely conductingfluidflowandinfinitely conductingfluidflow as applica- tionsofcorrolaries and
II
respectively.FINITELY CONDUCTING FLUID.
EliminatingL*, J*, WI*, W:*
frOIll equations(46), (,t7)
and(48)
by using($2) and(83),
wcfindthat F(q) andf*(q,O) mustsatisfyq
Of*
f’w*
-t F"(q)Oq
I-Kl*a
0(84)
of"
=0(85)
00
w_"(q) ]’
0(86)
w*’(q) + F’(q)
F"(q)J
sothat F(q)is the Legendretransform function ofastreamfimction. Here w*(q) isgivenin
(83)
and j* -Kp*ahas been usedforthefinitelyconductingcase. Since equation(86)isidentically satisficdwhenw* 0 andcan bercwrittenas
w*"(q) F"(q) F"’(q)
=0
(87)
w*’(q) F’(q)
F"(q)
when
w*’(q) #
O,it follows that wehaveto deal separatelywithL*(q,O)
F(q) havingvariable vorticityand L*(q,O) F(q) havingconstantvorticity.CASE1. (VariableVorticity). Fromtheexpressionsforx,y in
(83).
wehavev/ + v +/-F’(q),
dr+F"(q). (88)
dq Integrating
(87)
twice withrespect toq, weobtainw*(q)
MinlF’(q)l + M: (89)
I08 P.V. NGUYEN AND O.P. CHANDNA
where
M1
andM2
arearbitrary constants.Substituting forw*(q)givenin
(83)
into(89),
wegetq
+ r-r
dq4-(Mrtnr + Mr) (90)
since
F"(q) :it:
0and,therefore,Integrating the differential equation
(90),
wegetq
+
rent+
r+ (91)
where
M
is an arbitrary constant.Employing
(88), (91)
inequations(51)
and making useof the definitionsuqcosO,
v Ov 8uqsinOandw 0 0, weobtain
u(x
y) _y[_M_gn(x2 + y2) + (2M2 M ) Mz
M f.n(x: y ( 2M2- Mi) M
-4- + )+
4
+
---
,(,y)
-t,,( + y’-) + M=
Using expression forw*(q) from
(83)
inequation(84)
and makinguseof(85),wehave(92)
qF’(q)(q) + _K__p’a F,2(q)
02
f’(q,O) (q).
Integrating the above equation,weget
M4 K’aF’(q)
if(q,
8)
(q) (93)qF’(q) 2q
where
M4
is arbitrary constant.Substitutingexpressions for
F’(q)
and qgiven by(88)
and(91)
respectively intoequation(93),
weobtainf(x,y)
=M4 --4-(x
:+
)gn(x -4-+ (x +
4-Ma
2
+
4(94)
We
useu(x,y), v(x,y)
and l(z,y)givenby(92)
and(94)in
equation(3)
andobtain-M.ty
Kl*ayMz Kv*az)
(z,y)=
z
2+y---+
2’z
2+y’- 2(95)
HODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS 109
Usingj
-#’oK,
equations(92), (94)
in equations(5)
and(6)
and integrating, we get e(z,y). Employingthis solutionfore(z,y) and(92)
in(1),
the pressurefunctionisdeterufined to bewhere
Ms
is anarbitrary constant.(96)
CASE2.
(Constant
Vorticity).Usingw* w0 constantinthe expression for w* givenin
(83),
wehaveqF"(q) + F’(q) -woF’(q)F"(q)
O.(97)
Integratingequation(97)
with respecttoq, wegetwoF"(q) 2qF’(q) + 2Me
0(98)
where
Me
is an arbitrary constantand if0 0thenMe #
O.Substitutingfor F’(q)givenby
(88)
intoequation(98)
andsolvingfor q,we obtain[wo V/’2 M6 +
Vi]
q=+ -V/+y + (99)
Thesolutionfor
.f*(q,O)
satisfyingequations(84)
and(85)
isgivenby(93),
wherenowqis givenby(99).
We
proceedasin variable vorticitycaseandobtain ,(,y)-v
- +
May k#"
ayMz
z2
+
V+
2’z
+V
II0 P.V. NGUYEN AND O.P. CHANDNA
and
where
M7
isan arbitrary constant.+ M7
(100)
INFINITELY CONDUCTING FLUID.
Employing the expressions forL , J’, W*, W*, F{
andF2*
asgiven by(83), (84), (44)
and(45)in
equations(47), (49),
we find that F(q) and f*(q,O)must satisfy
O0 0
(101)
LF" 2’f"
-0.Solving
(101), (102),
weobtainl’(q, 0)
(102)
(103) where
isan arbitrary function ofitsargument,andF(q)
satisfyingF"/ 0.
(104)
Analysingequation
(104),
wehave thefollowingtwocases asinfinitely conductingfluidflow:(1) L*(q,O) F(q)
havingvariable vorticity.(2) L*(q,0)
F(q) havingconstant vorticity.CASE
1.(Variable
Vorticity). Followingthe sameanalysis as in finitelyconductingfluid flow,weobtain q,
u(z,y), v(z,y), w(z,y)
as givenby(91)
and(92). Hence,
f(x,y) (q) (105)
where qisgivenby
(91).
Proceedingasinpreviousexample,weget
M/n(z y
j(z,y)
=(q)
- + + U
+ ’(q)[--,n(z’ +yZ)+ (2M:
4)-M1
Ma M x + y:tn(z + y2)
g(x,y) (q)(u(x,y),v(x,y))
(106)
(107)
HODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS iii
p(z
V) =gu
PM+--- M1cz +2 [tn(z + V:
(MIM2-M?) y2]
+
pMM (z+
MM
2 4[t. * + u*)] + +- u,u . +
[ (2M=-M) M
+
aM tn(
x+ y= +
4
+
z
+ y=
3 + 2a M 4M M M
+
2+ (z+y} z+y +Ms
where
Ms
is arbitrary constt andj,H, H2
even
by(106), (107).
CASE
2.(Constant
Vorticity).In
tsce, usingL*(q,)
F(q)having constantvorticity w*w0, and
f*(q,8)
(q), weobtn q, u(x,y),v(x,y) ven
by(99)
andin(100),
f(x,y)where qisnow
ven
by(99),
(.,) () + ’() V +
*4. +
2](x,y) (q)(u(x,y),v(x,y)) (110)
[w
8woM6tn(x
yM woM6
P(’) = + * ( [f
jH.d+ )+ + -- f jH.dy] + + 6a (’ )- + + 2(. 4a)M u’)’ + )
2(111)
where
M
is arbitraryconstant,and j,H, Hz
areiven
by(109), (110).
Sumng
up,wehave thefollowingtheorems:TaEOREM VII.
H
L*(q,8) F(q) is theLegendre ransformfunction ofastreamfunction forasteady, plane, Migned, incompressible,nitclyconducting second-gradeBuidBow,
then theBow
in thephysicM planeis() . ln(x
by,o. + y2)
constant(). () o ()
itsstreauHincs, when vorticity( + u) [ut(,.
is+
notu:)+
a constant.M] + (b)
given byequations(100)
havingwo(x + y) + 2Mn(x + y2)
constant itsstrearines, when vorticityisaconstant.
THEOREM VIII.
H
L*(q,O) F(q)is theLegendre transformfinction ofastreamfinction /’orasteady, plane,aligned,incompressible, intlnitely conductingsecond--gradefluid flow,the flow in thephysicMplaneis(a)
given byequations(92), (105)
to(108) having(z: +y2) [_tn(z + y:) + -P.t +
tn(z + y)
constantasitsstreamlines, when vorticityisnota constant.(b)
given byequations(100), (109)
to(111)
withw0(x: + y-) + 2Mtn(z + y:)
constantasitsstream/ines, when vorticityis aconstant.
I12 P.V. NGUYEN AND O.P. CHANDNA
APPLICATION
IV.Let
L*(q,O)
AO+ B (112)
be theLegendretransform function, where
A, B
arearbitrary constantsandA
isnonzero.Weevaluate
J*,
to*,W*, W
by using(112)in
equations(40)
to(43)
and obtainJ*
q4
A2
W* W*
0.(113)
FINITELY
CONDUCTING FLUID.
Employing(112), (113)
inequations(46), (47)
and(48),
wefindthat equation
(48)
isidenticallysatisfied andf*(q,8)
mustsatisfyO I__* AK I’_______o
O0 q2
/ (114)
0/*
0 Solvingequations(114),
weobtainf*(q,o) 4,(o)
wlmreanarbitrary functionb(O)
must satisfyq2b’(0) + AIr*oK
O.(115)
Equation
(115)
holds trueforall q if’(0)
0 andAK#*o
0. Therefore,wehavef* (q,O) (0) N (116)
where
N
is anarbitrary constant andK
0.Using
L*(q,O)
AO+ B
andf*(q,O)= N,
weobtain-V=(,v)= +,+
p(z,y) N2
2(** + y*) + (6a, + 4a2) z, + y- (117)
where
N2
is anarbitraryconstant.INFINITELY CONDUCTING FLUID.
EmployingL*, J*,
*,W, W, F
andF
#yen by(112), (113), (44)
and(45)
inequations(47), (49),
wefind that[*(q,O)
mustsatisfyof"
=o
o ()
of" o
OO
Solving equations(118),
weobtainI*(q,O) N3
where
Na
isanarbitrary constant.Proceedingas
before,
wehave thefollowingresults:./=0
HODOGRAPHIC STUDY OF STEADY PLANE FLUID FLOWS 113
p(x,y)
=N4-
2(x2+y:)
+(6ai +4a2) :+y (119)
where
N4
is anarbitraryconstant.Summingup,wehave thefollowingtheorem.
TnwORWM
IX.
IfL*(q,O)
AO+ B
isthe Legendretransformfunctionofastreamfunction /’orasteady, plane, aligned, incompressible,Iniielyconductingsecond-grade
auidSow,
then the aowinthephysical planeisgiven byequations(117)
withtan-1()
constantasitsstreamlines.TrlEORIM X. If
L(q, O) At + B
isthe Legendretransform function ofa s/reamfunction for asteady, plane, a/igned, incompressible, in6nitelyconducting second--gradeBuidttow,
then the flowin the physicalplaneis given byequations(119)
havingtan- ()
constant as itsstream/ines.
REFERENCES
1.W. F. Ames,"Non-linearpartialdifferentialequations,"AcademicPress, NewYork, 1965.
_9.A. M. Siddiqui, P. N. Kaloni andO. P.Chandna, Hodograph fransfo,’mafton,ncfhods ,on-Neu, tontan fluids, J.ofEngineeringMathematics11(1956),203-216.
3.O. P.
Ch---n-clna,
R. M. Barron andA.C.
Smith, Rotationalplaneflows of vtscousflutd, Sia,nJ. Appl.Math.
4
(1982),1323-1336.4.M.H.Martin, Theflow