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Internat. J. Math. & Math. Sci.

VOL. 17 NO. (1994) 155-164

FLOWS FOR CHOSEN VORTICITY FUNCTIONS-- EXACT SOLUTIONS OF THE NAVIER-STOKES

EQUATIONS

155

O.P. CHANDNAandE.O.OKU-UKPONG

Department

of Mathematicsand Statistics

and

FluidDynamics ResearchInstitute University of Windsor Windsor, Ontario, Canada N9B 3P4

(Received April 30, 1992)

ABSTRACT. Solutions areobtainedfortheequationsof the motionof thesteadyincom- pressibleviscousplanar generalizedBeltrami flowswhenthe vorticity distributionisgiven by

V2b + f(z,y)

for threechosen forms of

f(z,).

KEY

WORDS

AND

PHRASES. viscousflow,asymptoticsuctionprofile,Beltrami flow.

1991AMS

MATHEMATICS

SUBJECTCLASSIFICATION CODES. 76 Fluid

Me-

chanics,35 Partial DifferentialEquations.

1.

INTRODUCTION.

Onlyasmall number of exact solutions of the Navier-Stokes equations has been found and Chang-Yi

Wang [1]

hasgivenanexcellentreview of these solutions. Theseknownsolutionsot viscousincompressibleNewtoaianfluids may be classifiedintothreetypes:

(i)

Flows for which the non-linearinertiaterms inthe linear momentum equations vanish identically. Parallelflowsand flows with uniformsuction areexamplesof these

flows;

(ii)

flowswithsimilarityproperties such that theflowequationsreducetoaset of ordinary differential equations. Stagnationpoint flowis anexample ofsuch

flows;

(iii)

flowsforwhichthe vorticity functionis sochosen that the governing equationinterm of the stream function reduces toalinearequation. Taylor

[2], Kampe

de Feriet

[3], Kovasznay [4], Wang [5]

and Lin and Tobak

[6] employed

this

approach,

taking

V2, K,, V, f().

V, + (K 4x),, V2, A + Cy

and

V K( Ry),

respectively.

In

this paper,westudy generalizedBeltrami flows when thevorticityfunction w

-Vb

isgiven by

V, + A

2

+ Bz + Cz + D, V2 , + Ay + Cz +D, Vb , + Cz

+Dy,

where

A,B,C,D

arereal constants.

(2)

2. BASIC

EQUATIONS

AND SOLUTIONS.

Steadyplaneincompressibleviscousfluidflow,inthe absence of external forces,isgoverned bythesystem:

+

0

1 P 1

(2.1)

where

(, ), f:(, 9)

axethe velocity

components,/5(,, 9)

thepressurefunction,p theconstant density,pthe constant viscosity and,2

r

0’

+

b

isthe Laplacian operator. Thevorticity functionforthisflowisgivenby

(2.2)

Letting

U,L

to be the characteristic velocity and length respectively, we introduce the non-dimensional variables

(2.3)

=Z, Y=Z, "=y, =y, =W, v-v,

in system

(2.1)

and equation

(2.2). We

apply theintegrability condition P-u Pu- to the linearmomentum equationsto find that u, v,w must satisfy the system:

(2.4)

where

R

L isthe Reynolds number.

Introducingthe stremfunction

(z, y)

suchthat

,.=,, v=-,

insystem

(2.4),

wefindthat

(z,y)

must satisfy

V@ + R 0(, Vb)

0

0(,)

In

this paper,westudyflows for which the vorticity distributions take theforms

w

-V2 -( + Ay

m

+ Bzy + Cz + Dy)

(b)

w

-Vb -( + Ay + Cz + Dy)

., -V2 -( + Cz + Dy)

where

A, B, C, D

arereal constants.

Form (a):

Substituting

(2.7)

inthe compatibility equation

(2.6),

weget

R(2Ay + Bz + D), R(By + C). + /, + Ay + Bzy + Cz + Dy +

2A 0

(2.8) (2.9)

(2.10)

(3)

EXACT SOLUTIONS OF THE STEADY NAVIER-STOKES EQUATIONS 157

Employingthecanonical coordinates

Ay

2

+ Bzy + Cz + Dy, = (2.)

where

(By + C) # O, (2.10)

maybewrittenas

-( + c). + + +

2A 0.

Thisequationissolved to obtain

f()(By + D):" (Ay + Bzy + Cz + Dy + 2A) (2.13)

where

f

isanaxbitrary function of

.

Introducing

(2.13)

into

{2.7),

weget

{R’ [C’(C’ + D’) + 2BCD( + B’(’] /"() + 2R[C(RAC + D)- B(] /’() + [1 RB- RC ] ()} + 2RC{2R[C(AD + BC)+ AB] f’()

+

2A

[RB + 1] f() RB/(()}. + R {2R [C(2A +

3B

) + ABCD

+ 4RC { [A + ]/"(0}.’ + R { [ + ]/"(0}.’

0

Since

,

eindependent vables d

{I, , , ,

isaHnely independent t,itfollows that the ccients of the

vous

powersof zero.

Tng

the coecients of

, s, ,

d1

equM

to zero,weget

(2.14)

f() cI + c (2.15)

2A(RB

+ 1)cl RBc

RBc,( 0

(2.16)

wherecl,

c

axearbitrary constants. Since

{1, }

isalinearlyindependent set,itfollows from

(2.16)

that

2A(RB + 1)cl RBc2 O, RBcl

0 giving

c c

0. Usingc,

c

0in

(2.15),

weobtain

f(()

0.

From

(10),

the streamfunction isgivenby

@(z, y) -(Ay’ + Bzy + Cz + Dy + 2A) (2.17)

The exact integral ofthisflowis

u=-(2Ay+Bz+D), ,=By+C,

and 1

[B(z2 + y,) + 2(BD 2AC)z + 2BCy]

p= po

- (2.18)

wherep0 is anaxbitraryconstant.

Equation

(2.17)

represents an impingement of two constant-vorticity oblique flows with stagnation point

(Z,Y)--<

2AC-BD

,

,-

) (2.9)

(4)

fornon-zero values of

A, B,

Cand E. The stagnation pointshifts upward as

B

gets smaller forfixedvaluesof

A,

Cand

E.

Weremark that when

A B

-1,

C D

0,the solution

(2.17)

reducestooneof the flows in

Wang’s [1]

paper.

Form

{b):

Employing

(2.8)

in

(2.6),

weobtain

R(2Ay

+ D)b, RCI, + + Ay

2

+ Cz + Dy +

2A 0

(2.20)

Choosingthe canonical coordinates

Ay

2

+ Cz + Dy,

I Y

(2.21)

whereC

#

0,

(16)

takes theform

-RCl,, + P + +

2A O.

(2.22)

We

solve this equation toget

=g()expIcy ) (Ay2 + Cz + Dy + 2A)

whereg isanarbitraryfunctionof

. We

substitute

(2.23)

into

(2.8)

toget

[R:C’ g"(,) + 2RAC g’(,) + (1 R:Cg()] + 2RCg’()(2Ar + D)

+ R2C2g"()(2Arl + D)

0

(2.23)

(2.24)

Since

,

1areindependent variables and

{1, (2A/+ D), (2A/+ D)

2

}

isalinearly independent set,itfollows that

g"() O, g’(6)

0,

(1 R2C)g()

0

(2.25)

From (1 RCZ)g()

0, we get the three possibilities:

g() =.0, R2C #

1;

R2C

2 1,

g(O #

0;

g(O o, R’C .

Thestream function

(2.23)

isgiven by

-(Ay +Cz+Dy+2A)

;g=O,

R 2C 2#1

,/,(,) ge g0 ( + 6’ + + z);6 ’ , #

-(A +6’+D+A)

;=0,

R 6’=1

whereg

#

0impliesg

K (non-zero constant).

Whenthestreamfunction isgiven by

(2.26)

,(z,y)--(Ay

/

Cz + Dy + 2A); RC

--1 or

RC #1, (2.27)

the exactintegralforthe flowis

u

-(2Ay + D),

v

C,

and p po

+

2ACz

(2.28)

(5)

EXACT SOLUTIONS OF THE STEADY NAVIER-STOKES EQUATIONS 159

wherep0isan arbitrary constant.

Thesolution

(2.28)

maybe realizedonaplatesituated

along

y

-

with uniform suction or blowing.

C >

0 andC

<

0,respectively, for blowingandsuction attheplate.

The exactintegralfor theflow givenby the stream function

(z,y)

Kexp (---V) -(Av2 +Cz + Dy + 2A); R

C2 1

(2.29)

is

u=-exp

V

(2Av + D),

v

C,

and p po

+

2ACz

(2.30)

wherep0is anarbitrary constant.

If

K

RCD in

(2.29)

and

(2.30),

the velocityprofilein

(2.30)

canberealizedon aplate

locatedalongV 0with uniformsuction. The velocity profileattains the form

(2.31)

onlyasymptotically, andsomay beregardedasthe asymptoticsuctionprofile

[7].

C

>

0 and C

<

0 forblowing andsuctionatthe plate, respectively.

Form

(c):

Substitution of

(2.8)

into

(2.6)

yields

RD. RCCu + + Cz + Dy

0

(2.32)

Thecanonicalcoordinates

=Cz+Dy,

7=V;

C:f-0 (2.33)

areemployedin

(2.32)

toget

-RC + + o.

Thesolutionofthisequationis

b h()exp (cy) -(Dz+Ey)

wherehisanarbitraryfunctionof

.

We employ

(2.34)

in

(2.9)

toobtain

R2C2(C

2

+ D-)h"() + 2nCDh’() + (1 n2C2)h()

0

(2.34)

(2.35)

Thegeneralsolutionof

(2.35)

is

h(O

A1 exp(Al) + A2 exp(A2)

(B1

Ci Cos(m( + C)

exp

;R2(C + D )-

1

>

0

R2(C

2

+ D )-

1 0

;R:(C

:

+ D )

1

<

0

(2.36)

(6)

where

-D + Cv/R2(C

:

+ D )

1

V/1 R2(C +

D

’)

A1.2 RC(C + D,)

m

R(C2 +

02

(2.37)

and

A,A=,B,B=,C,C=

ebitryconstts.

Wesh study the three possibiHtiessepately.

(i) R(C + D )-1>

0

The strefunction,

om (2.34)

d

(2.36),

is

(z,y) A

exp

[ACz + (2D+ )yl + A,

exp

[A,

Cz

+ (A,D+ )y]-(Cz+Dy)

(=.3s)

TheexactintegrMoftsflowis

u=

(D+ )A

exp

[ACz + (D+ )y]

+ (2D+)A,

exp

,C+ (A2D+)yI-D,

v

-D {lA

exp

[Cz + (D + ) y] (2.39)

+

2Aexp

and

P=po

+

2 1-

R,(C,

+

O2

A1A2exPtR-- +

wherep0 isanarbitrary constant and

A1

,2 aregiven by

(2.37).

Ts

flow reprents impingement of obquefo stre th obfique rota- tionM,

vergent flow,

th stagnation point

(z,y)

2,(C + D’)-

1

DR’(C’ + D’)

l

m { -4AA’[R’(C’ + D’) I]

}

a=(C + D)=

R(C + D) 2.40)

whereA,A2 enon-zero

mM

constants deither

A >

0,

A <

0or

A <

0,

A2 >

0.

Fo

ed

ues

of

R,

Cd

D,

the stagnation point sftsupwdwhenthe absolute vMueof

A

islgerth that of

A.

H A

d

A

areofthesesign, the abovephenomenonds not

te

plce,dwehave aflow thouta

staation

point.

(ii) Rx(C ,

+ D =)-1=0

Using

(2.36)

in

(2.34),

the stre functionis

(z,V) [Bx + B2(Cz + DV)]e[R(OV- D)]- (C + Dr) (2.41) Ts

flow h theexitintegrM

u

{DB2 + RC[Bx + B2(Cx + Ov)]}exp[R(CV- O,)]- E,

v

{-DB2 + RD [Bx + Bx(C + Oy)]}

exp

[R(Cy- D)] + D,

d

(2.42)

1

(7)

EXACT SOLUTIONS OF THE STEADY NAVIER-STOKES EQUATIONS 161

wherep0 isan arbitrary constant.

If

B2

isapositive realconstant,thisflow representsanimpingement ofanoblique uniform streamwithanoblique rotational,divergent flow,with stagnation point

1

(CB1

(z,t/) -C +

D2

B2

D In

B2,

DB

C

)

R + In B, (2.43)

Forfixed values of

R

and

C,

the stagnation point shifts upwardif

B1

and

D

areof opposite signs and the absolute value of

B1

islargerthan

If

B2

isanegative realconstant,

(2.41)

representsanoblique uniform streamwhich abuts on anoblique rotational,convergent flow.

(iii) R 2(C2+D2)-1<0

From

(2.27)

and

(2.36),

the stream functionisgivenby

{’z,y) C,

Cos

[m(Cz +

Dy)

+ C2]

exp

Cv- Dz _(Cz +

Dy)

R(C + D 2) (2.44)

The exactintegral forthisflowis

{

CCos

[m(Cz + Dy) +

R(C

2

+ D 2)

Cy-

Dz -mRD(C + D2)Sin [m(Cz + Dy) + C2]}

exp

R(C2 +

02

D,

v

R(C2 +

02

{DCos [m(Cz + Dy) + C,] (2.45)

+mRC(C + D2)Sin[m(Cz +

Dy)

+ C2]}

exp

[R(C

2

+

D2

+ C,

2(Cv Dz) R(C + D =)

1 1

]C21Cos2[m(Oz+Dt/)+O2]ex

p

P0+

1-

R=(C = +

D2

and

whereP0 isanarbitraryconstant,andmisgivenby

(2.37).

If

Cx >

0,the stagnation points forthisflowaxe

( RC[(2n + I){ C:] [C1v/1- R2(C: + D2’i]

(=,y)

----R(b ..D-) + RDIn R(C2 + D2) RD[(2n+I);-C2]

X/1 R2(C + D’)

RCln

R(C2 +

D2

(2.46)

wheren isaninteger.

Fig. 1 shows the streamlines for

(z,y) -(Av

2

+ Bzt/+ Cz + Dy + 2A)

when

A B C D

1. Figures 2 and 3 represent the flows

tk(z,y) -(Ay

2

+

Ca:

+ Dy + 2A)

and

(z,t/) K

exp

(cY) (At/2 + Cz + Dt/+ 2A)

for

K R A C D

1. Figures4 and 5 illustrate thecase

(c) (X72 +

Cz

+ Dt/)

when

R2(C

2

+ D 2) >

1. Figure4 shows reversedflow.

C=D=I,R=2, Az

=50,

A2

=60andC=D=R=l,

A1

=1,

A2=-1,

respectively,forFigures4 and 5. The flows when

R2(C

2

+ D 2)

1 aregiveninFigures 6 and

7whenC=D=l,R= ,B1

=50,

B2=-60andC=D=l,R=,Bt

=0,

B2=l.

WhenR

(C 2+D2)<1.

wehave

Figure8forC=D=l,R=1/2, Cx

=5,

C2=0.

(8)

Figure 1

-0. l0

55

-.00

-o.o -I.$ -s.@ .s

Figure 2

Fibre

3

-;0

-0

-40

o

o 4o

F]x

4

(9)

EXACT SOLUTIONS OF THE STEADY NAVIER-STOKES EQUATIONS 163

oo BO

Fibre

5

-’O.O

-tS.O -?.$ 15.0 Io

(10)

REFERENCES

[1]

C.-Y. WANG Exact solutions of the steady-state Navier-Stokes equations,

Annu. Rev__._:

Fluid Mech. 23.

(1991)

159-177.

[2]

G.I. TAYLOR On thedecay ofvortices ina viscousfluid,Phil.

Mag:, Serie....__.s

6,46

(1923)

671-674.

[3]

J.

KAMPE DE FERIET

Sur quelques casd’integration des equations du mouvementplan d’unfluide visqueux incompressible,

Proc_._._: Int._._:..Congr.

Appl.

Mech.._...:, 3rd_._.:.

Stockholm 1_

(1930)

334-338.

[4] L.I.G. KOVASZNAY

Laminarflow behindatwo-dimensional grid,

Proc_.

CambridgePhil.

Soc_. 44,

(1948)

58-62.

[5]

C.-Y. WANG

On

a class ofexact solutions of the Navier-Stokes equations,

J__.

of

Mech. 33

(1966)

696-698.

[6]

S.P. LIN and M. TOBAK Reversed flow abovea plate withsuction,

.AIAA_,

24,

No.

2.

(1986)

334-335.

[7]

H. SCHLICHTING

.Boundary-Laye ,

McGraw-Hill, 1968.

(11)

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