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Applied Mathematics E-Notes, 11(2011), 133-138 c
Available free at mirror sites of http://www.math.nthu.edu.tw/ amen/
ISSN 1607-2510
Traveling Wave Solutions of Burgers’Equation for
Power-Law Non-Newtonian Flows
Dongming Weiy, Harry Bordenz
Received 30 June 2010
Abstract
In this work we present some analytic and semi-analytic traveling wave solutions of a generalized Burgers’ equation for unidirectional ‡ow of power-law
non-Newtonian ‡uids. The solutions include the corresponding well-known traveling wave solution of the Burgers’equation for Newtonian ‡ows. We also derive
estimates of shock thickness for the power-law ‡ows.
1
Introduction
In this work, we are interested in …nding traveling wave solutions to the following
generalized Burgers’equation for power-law ‡uid ‡ows
!
n 1
@u
@u
@
@u
@u
+u
=
(1)
@t
@x
@x
@x
@x
where is the density, the viscosity, u the velocity of the ‡uid in x direction, and
n 6= 1 the power-law index. For n = 1, (1) reduces to the famous Burgers’equation for
Newtonian ‡ows
@u
@u
@2u
+u
:
(2)
=
@t
@x
@x2
It is well-known that if we impose boundary conditions
lim u( ) = u2 ;
! 1
lim u( )) = u1 ;
!+1
lim
j j!+1
u0 ( ) = 0;
where u2 > u1 , then (2) has the following celebrated traveling wave solution
u( ) =
u1 + u2 exp[
1 + exp[
2
2
(u1
(u1
u2 )]
u2 )]
(3)
where = x
t, u1 and u2 are downstream and upstream ‡uid velocities respectively.
It can be shown that there exists of a thin transition layer of thickness in the order
Mathematics Subject Classi…cations: 35L67, 76A10, 35Q53.
of Mathematics, University of New Orleans, New Orleans, Louisiana 70148, USA
z Department of Mathematics, University of New Orleans, New Orleans, Louisiana 70148, USA
y Department
132
D. M. Wei and H. Borden
133
of u22 u1 for ‡ows de…ned by (3). This thickness can be referred to as the shock
thickness, which tends to zero as ! 0 , and for …xed , ! 1 as (u2 u1 ) ! 0.
See, for example, [6] or [7] for derivation of (3) and analysis of (2). In this work, we
…nd analytic and semi-analytic solutions to (1) for various values of n, and we derive
the corresponding order of thickness for the transition layers in the power-law NonNewtonian ‡ows. Applications power-law ‡ows are abundant in studying of ‡ows in
glacier, blood, food, oil, polymer etc., see e.g. [3]. There are numerous papers denoted
to study equation (2) in the literature for understanding shock formation and traveling
waves in Newtonian ‡ows dating back to the original papers of Burgers, Hopf, and Cole,
see [6], [8], and [9]. A generalized Burgers’ equation for Non-Newtonian ‡ows based
on the Maxwell model has recently been studied in [7] recently. In this work, we will
show that the corresponding traveling wave solutions to (1) with the same boundary
conditions can be implicitly de…ned by
1
2
1
n
(u2
u)
=
u u1
u2 u 1
1=n
2 F1
1
n )[(u
(1
1 u2 u
n ; u2 u1
1 1
n; n; 2
1
1
u1 )(u2
u)] n
and the …rst order approximation of the thickness of the transition layer is
(u2
u1 )
1=n
8
(u2
:
u1 )2
This result extends the classical result from n = 1 to n 6= 1. We have not found any
paper in the literature which deals with the power-law Burges’s equation (1) for n 6= 1.
2
The Generalized Burgers’Equation for Power-Law
Fluid Flows
The general Navier-Stokes equation for incompressible viscous ‡ows is given by
D~u
=r ~
Dt
where ~u = (u1 ; u2 ; u3 ) is the ‡uid velocity,
0
1
=@
11
12
13
21
22
23
31
32
33
rp + ~g
0
A and D~u = @
(4)
11
12
13
21
22
23
31
32
33
1
A
are the stress and strain tensor, the density, p the scaler pressure, and ~g the external
@u
@ui
+ @xji ); 1
i; j
3: For unidirectional ‡ows, we assume that ~u =
force, = 12 ( @x
j
@p
(u1 ; 0; 0); ij = 0 for i 6= 1 or j 6= 1; ~g = (g1 ; 0; 0); and rp = ( @x
; 0; 0): The Navier1
Stokes equation (4), in this case, takes the following simple form
Du1
@ 11
=
Dt
@x1
@p
+ g1
@x1
(5)
134
Traveling Wave Solutions of Burgers’Equation
@u1
@u1
1
where Du
Dt = @t + u1 @x1 :
Rheological relationships between and D~u are frequently used to determine the
type of ‡uids. It is well-known that for power-law ‡uids, the rheological relation is
given by
(n 1)=2
i; j 3
(6)
ij = 2Kj2 kl kl j
ij ; 1
where n is called the power-law index, see e.g., [1] or [9]. If n = 1 , then the ‡uid is
said to be a Newtonian ‡uid, and it is non-Newtonian if n 6= 1. For many important
industrial polymer ‡uids, the value of n is between 0 and 1. Table1 provides values of
K and n for some important industrial power-law ‡uids:
Polymer
Nylon
Polystyrene
Polyethylene
Temperature (Kelvin)
493
463
453
K(P asn )
2:62 103
4:47 103
4:47 103
n
0:63
0.22
0.56
Table 1: Values of K and n
For the unidirectional power-law ‡ows, (6) reduces to 11 = 2n Kj 11 j(n 1) 11 . Let
u1 ; x1 ; g1 ; and 2n K be denoted by u; x; g and respectively. Then from (5), we have
the equation for the unidirectional power-law ‡ows
@u
@u
+u
@t
@x
=
@
@x
@u
@x
@p
+g
@x
(7)
@p
@x
+ g = 0, we then have
where (t) = jtjn 1 t; 0 < n < 1: In (7), let = , and let
the generalized Burgers’equation for power-law ‡uids
@u
@
@u
@u
+u
=
( )
@t
@x
@x @x
(8)
We are interested in …nding solutions of (8) for n 6= 1.
3
Traveling Wave Solutions
Let u(x; t) = u( ) , with
becomes
=x
t . Then
@u
@t
=
@u
@u
@
+u
=
@
@
@
@u @u
@ , @x
@u
@
Therefore,
@
@
1 2
u
2
u
du
d
=0
which gives
1 2
u
2
u
du
d
=A
=
@u
@ ;
and equation (8)
(9)
D. M. Wei and H. Borden
135
in which A is the integration constant. Applying the downstream and upstream boundary conditions: lim !+1 u( ) = u1 ; lim ! 1 u( ) = u2 ; limj j!+1 u0 ( ) = 0 we get
du
d
where
=
1 2
(u
2
= 12 (u1 + u2 ), and A =
du
=
d
1
Therefore
1
(u
2
Z
2 u
1
2 u1 u2 .
u1 )(u
1 ((u
2A) =
1
(u
2
1
Since
u2 )
du
u1 )(u
u2 ))
=
1
(t) = jtj( n
1
n
1
2
=
u1 )(u
Z
1
1
2
((u
1
n
u2 )
1)
t, we have
u1 )(u
u2 ))
d
(10)
Without loss of generality, in the following, we assume that u2 > u > u1 . For n = 1,
(10) gives
Z
1
du
1
u u1
=
=
ln
2
(u u1 )(u u2 )
u1 u2
u2 u
which gives the celebrated traveling wave solution
i
h
(u
u
)
u1 + u2 exp
2
1
2
h
i
u( ) =
1 + exp
(u
u
)
2
1
2
to the Burgers’ equation for Newtonian ‡ows. In the following, we are interested in
…nding solutions to (10) for n 6= 1. By using Mathematica, we …nd that
Z
1 ((u
du
u1 )(u
(u2
u2 ))
u)
=
u u1
u2 u1
(1
1=n
2 F1
1
n )[(u
1
1 u2 u
n ; u2 u1
1 1
n; n; 2
u1 )(u2
1
u)] n
(11)
where 2 F1 is the well-known Gauss hypogeometric function de…ned by the series
2 F1 (a; b; c; x) =
1
X
(a; k)(b:k)
k=0
(c; k)
xk ; jxj < 1
where (a; k) = a(a + 1):::(a + k 1) is the Appel symbol, see e.g. [2]. Therefore, from
(11), we have the following power series solution to the generalized power-law Burgers’
equation
s
1
1
k
n n (u2 u)n 1 X (1 n1 ; k)( n1 ; k) u2 u
1 n
=
;
2
n 1
u2 u1
u2 u1
(2 n1 ; k)k!
k=0
where n 6= 1; j uu22
u
u1 j
< 1:
136
Traveling Wave Solutions of Burgers’Equation
It is interesting to note that for some special values of n, the integral (10) can be
expressed in terms of elementary functions. In particular, for n = 12 , we have
Z
du
=
2
(2 )
((u u1 )(u2 u))2
1
1
u2 u
1
2
=
ln
+
+
2
3
(u2 u1 )
u u2
u u1
(u1 u2 )
u u1
for n = 13 , we have
Z
=
(2 )3
((u
+
du
u1 )(u2
u))3
)3
1
(u u2 )2
1
2(u1
u2
=
3
1
1
)4
(u2
u1
u u2
u u1
1
6
+
ln
(u u1 )2
(u2 u1 )5
u2 u
u u1
for n = 2, u2 > u > u1 , by using the identity z2 F1 (1=2; 1=2=; 3=2; z 2 ) = a arcsin z and
(11), we also get
Z
1=2
1=2
du
1
u2 u
u2 u
=
=
2
2 F1 1=2; 1=2=; 3=2;
2
u u1
u u1
((u u1 )(u2 u))1=2
=
2 arcsin
u2 u
u u1
1=2
respectively. Therefore, we have the following three traveling wave solutions for the
three special values of n:
(2 )2
(2 )3
=
1
(u2
=
(
u1 )2 u2
1
1
u
u
u1
)
2
(u1
u2 )3
ln
u2 u
u u1
1
1
1
1
(
+
)+
u1 )4 u2 u u u1
2(u2 u1 )3 (u u2 )2
6
u2 u
ln
(u2 u1 )5
u u1
; for n =
3
(u2
for n = 13 ; and
1
2
1=2
= 2 arcsin
u2 u
u u1
(u
1
;
2
1
u1 )2
1=2
for n = 2
More analytic solutions in terms of elementary functions for special values of n can
be derived and they are not listed here due to limited spaces. We have omitted the
integration constants in the above solutions. For simplicity, let u1 = 1; u2 = 1;
pro…les of the transition layers for three special cases are given in Figure 1, with u
versus ( 21 )1=n : These three cases represent Newtonian (n = 1), Non-Newtonian shearthinning (n < 1), and Non-Newtonian shear-thickening ‡uid ‡ows (n > 1) respectively.
In Figure 1, solid thick line represents the Newtonian ‡uids, the solid thin line
represents the shear thickening ‡uids, and the dash line represents the shear thinning
‡uids.
D. M. Wei and H. Borden
137
0.5
1.5
1.0
0.5
0.5
1.0
1.5
0.5
Figure 1: Transition layers
4
The Order of Thickness of the Transition Layers
The transition layer thickness or the shock thickness can be estimated by using the
…rst order derivative du
d (0). From
du
=
d
and u(0) =
u1 +u2
2
1
1
(u
2
u1 )(u
u2 )
1
n
1
((u
u1 )(u
u2 ))
we get
du
(0) =
d
Let
1
2
=
u1 )2
(u2
1=n
8
denote the thickness of the transition layer. Using the Taylor expansion, we have
u2
u1
u
2
u
2
=
du
(0) + O( 2 )
d
Therefore, we have
= (u2
u1 )
8
1=n
(u2 u1 )2
which is the …rst order approximation of the thickness of the transition layer for the
power-law ‡ows. This estimate, for n = 1, gives the well-known estimate for the
thickness of the transition layer of the Newtonian ‡ows.
5
Conclusions
In this work, we have derived a generalized Burgers’equation for the power-law ‡ows,
and we also derive a new general traveling wave solution of this equation in terms of
138
Traveling Wave Solutions of Burgers’Equation
the Gauss hypergeometric function. As special cases of this general solution, we show
several analytic solutions in terms of elementary functions as well as the pro…les of
the transition layers of the solutions. We de…ned a …rst order approximation of the
thickness of the transition layer or thickness of the shock for the generalized Burgers’
equation. The results generalize the known solution and shock-layer estimate for the
Newtonian ‡ows.
References
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Journal of Scienti…c Research, ISSN 1450-216X, 34(1)(2009), 55–60.
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Vol. 1–2 Wiley, New York, 2nd ed., 1987.
[4] J. M. Burgers, J. M. A mathematical model illustrating the theory of turbulence.
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Mechanics, 171–199. Academic Press, Inc., New York, N. Y., 1948.
[5] V. Camacho, R. D. Guy and J. Jacobsen, Traveling waves and shocks in a viscoelastic generalization of Burgers’equation, SIAM J. Appl. Math., 68(5)(2008),
1316–1332.
[6] J. D. Cole, On a quasilinear parabolic equation occurring in aerodynamics, Quart.
Appl. Math., 9(3)(1951), 225–236.
[7] Lokenath Debnath, Nonlinear Partial Di¤erential Equations for Scientists and
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[9] E. Hopf, The Partial Di¤erential Equation ut + uux = uxx , Comm. Pure and
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