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for
11.4 Two-Dimensional Mathematical Models
We now consider problems involving steady state heat flow, electrostatics, and ideal fluid flow that can be solved with conformal mapping techniques. Conformal mapping transforms a region in which the problem is posed to one in which the solution is easy to obtain. As our solutions involve only two independent variables, x and y, we first mention a basic assumption needed for the validity of the model.
The physical problems we just mentioned are real-world applications and involve solutions in three-dimensional Cartesian space. Such problems generally would involve the Laplacian in three variables and the divergence and curl of three-dimensional vector functions. Since complex analysis involves only x and y, we consider the special case in which the solution does not vary with the coordinate along the axis perpendicular to the xy plane. For steady state heat flow and electrostatics, this assumption means that the temperature, T, or the potential, V, varies only with x, and y. Thus for the flow of ideal fluids, the fluid motion is the same in any plane that is parallel to the z plane. Curves drawn in the z plane are to be interpreted as cross sections that correspond to infinite cylinders perpendicular to the z plane. An infinite cylinder is the limiting case of a "long" physical cylinder, so the mathematical model that we present is valid provided the three-dimensional problem involves a physical cylinder long enough that the effects at the ends can be reasonably neglected.
In Section
11.2 and Section 11.3, we
showed how to obtain solutions
for harmonic functions. For applications, we need to
consider the family of level curves
(10-16) ![]()
and the conjugate harmonic function
and
its family of level curves
(10-17) ![]()
For convenience, we introduce the term complex potential for the
analytic function
.
We use Theorem 11.4, regarding the orthogonality of the families of
level curves (10-16) and
(10-17), to develop ideas concerning the
physical applications that we will consider.
Theorem 11.4 (Orthogonal Families of
Level Curves). Let
be harmonic in a domain D. Let
be the harmonic conjugate and let
be
the complex potential. Then the two families of level
curves given in
Equations (10-16) and
(10-17), respectively, are orthogonal in
the sense that if
is a point in common to the two curves
and
, and if
, then these two curves intersect orthogonally.
Proof of Theorem 11.4 is in the book.
Complex
Analysis for Mathematics and Engineering
The complex
potential
has
many physical interpretations. Suppose, for example, that
we have solved a problem in steady state temperatures. Then we can
obtain the solution to a similar problem with the same boundary
conditions in electrostatics by interpreting the isothermals as
equipotential curves and the heat flow lines as flux lines. This
implies that heat flow and electrostatics correspond directly.
Or suppose that we have solved a fluid flow problem. Then we can obtain a solution to an analogous problem in heat flow by interpreting the equipotentials as isothermals and streamlines as heat flow lines. Various interpretations of the families of level curves given in Equations (10-16) and (10-17) and correspondences between families are summarized in Table 11.1.
Table 11.1 Interpretations for the level curves of
and
.
Preview of Applications
The following is a sample of applications
taken from Section
11.5 Steady
State Temperatures; Section
11.6 Two-Dimensional
Electrostatics; Section
11.7 Two-Dimensional
Fluid Flow; Section
11.8 The
Joukowski Airfoil ; Section
11.9 The
Schwarz-Christoffel Transformation; Section
11.10 Image
of a Fluid Flow; Section
11.11 Sources
and Sinks.
Example 11.16. (See
Section 11.5 for more.) Find the
temperature
at each point in the upper half-disk
, if
the temperature at points on the boundary satisfies
![[Graphics:Images/MathModelsMod_gr_68.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_68.gif)
Solution. As discussed in Example 11.9, the
transformation
![]()
is a one-to-one conformal mapping of the half-disk H
onto the first quadrant
,
and can be written as
(11-24)
The conformal map given by Equation
(11-24) gives rise to a new problem of
finding the temperature
that satisfies the boundary conditions
![[Graphics:Images/MathModelsMod_gr_73.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_73.gif)
If we use Example 11.2, the harmonic function
is given by
(11-25)
.
Substituting the expressions for u and v from Equation
(11-24) into Equation
(11-25) yields the desired
solution:
.
The isothermals
are
circles that pass through the points ±1, as shown in Figure
11.19.
Figure 11.19 The temperature
in a half-disk.
Example 11.21. (See
Section 11.6 for more.) Find the
electrical potential
in
the disk
that
satisfies the boundary values
![[Graphics:Images/MathModelsMod_gr_91.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_91.gif)
Solution. The mapping
is
a one-to-one conformal mapping of D
onto the upper half-plane
with
the property that
is mapped onto the negative u axis
and
is mapped onto the positive u
axis. The potential
in the upper half-plane that satisfies the new boundary values
is given by
(11-29)
.
A straightforward calculation shows that
![[Graphics:Images/MathModelsMod_gr_99.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_99.gif)
We substitute the real and imaginary parts,
and
from
this equation, into Equation (11-29) to
obtain the desired solution:
.
The level curve
in
the upper half-plane is a ray emanating from the origin, and the
preimage
in
the unit disk is an arc of a circle that passes through the
points
. Several
level curves are illustrated in Figure 11.38.
Figure 11.38 The potentials
and
.
Example 11.24. (See
Section 11.7 for more.) Find the
complex potential for an ideal fluid flowing from left to right
across the complex plane and around the unit
circle
.
![[Graphics:Images/MathModelsMod_gr_120.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_120.gif)
Solution. We use the fact that the conformal
mapping
maps
the domain
one-to-one
and onto the w plane slit along the segment
. The
complex potential for a uniform horizontal flow parallel to this slit
in the w plane is
,
where A is a positive real
number. The stream function for the flow in the w plane
is
so
that the slit lies along the streamline
.
The composite
function
determines
the fluid flow in the domain D, where
the complex potential is
,
where
. We
can use polar coordinates to express
as
![[Graphics:Images/MathModelsMod_gr_131.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_131.gif)
The streamline
consists
of the rays
and ![]()
along the x axis and the curve
, which
is the unit circle
. Thus
the unit circle can be considered as a boundary curve for the fluid
flow.
The approximation
is
valid for large values of z, so we can approximate the flow with a
uniform horizontal flow having speed
at
points that are distant from the origin. The
streamlines
and
their images
under
the mapping
are illustrated in Figure 11.51.
Figure 11.51 Fluid flow around a circle.
Example 11.27. (See
Section 11.9 for more.) Use
the Schwarz Christoffel formula to verify that
maps
the upper half plane
onto
the upper half plane
slit
along the line segment from
.
(Use the principal square root throughout.)
![[Graphics:Images/MathModelsMod_gr_172.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_172.gif)
Solution. If we choose
and
, then
the formula
![[Graphics:Images/MathModelsMod_gr_164.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_164.gif)
will determine a mapping
from the upper half-plane
onto
the portion of the upper half-plane
that
lies outside the triangle with vertices
as
indicated in Figure 11.73(a). If we let
, then
,
and
.
Figure 11.73 The region with
and
.
The limiting formula for the derivative
becomes
![[Graphics:Images/MathModelsMod_gr_176.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_176.gif)
which will determine a mapping
from the upper half-plane
onto
the upper half plane
slit
along the line segment from
as indicated in Figure 11.73(b). An easy integration
reveals that
is given by
and the boundary values
lead
to system of equations
and ![]()
the solution is easily found to be
and the desired function is
.
Example 11.29. (See
Section 11.10 for more.) Show
that the mapping
maps
the upper half plane
onto
the domain in the w-plane that lies above the boundary curve
consisting of the rays
and the segment
(see
Figure 11.87).
![[Graphics:Images/MathModelsMod_gr_206.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_206.gif)
Figure 11.87 (a) Flow over a step. (b) Flow around a blunt object.
Hint: Set
and
. In
the w-plane
,
and the exterior angles are
, and
the formula for the derivative
is
![[Graphics:Images/MathModelsMod_gr_212.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_212.gif)
Integrate and get
![[Graphics:Images/MathModelsMod_gr_213.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_213.gif)
Solve for the coefficients A and B and obtain
![]()
It maps the upper half-plane
onto
the domain in the w plane that lies above the boundary curve
consisting of the rays
and the segment
. Furthermore,
the image of horizontal streamlines in the z
plane are curves in the w plane given by the parametric equation
![[Graphics:Images/MathModelsMod_gr_218.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_218.gif)
for
. The
new flow is that of a step in the bed of a deep stream and is
illustrated in Figure 11.87(a). The function
is also defined for values of z in
the lower half-plane, and the images of horizontal streamlines that
lie above or below the x axis are
mapped onto streamlines that flow past a long rectangular obstacle,
which is illustrated in Figure 11.87(b).
Example
11.30. (Source and
sink of equal strength) (See Section
11.11 for more.) Let a source and sink of unit strength be
located at the points
and
,
respectively. The complex potential for a fluid flowing
from the source at
to
the sink at
is
.
![[Graphics:Images/MathModelsMod_gr_257.gif]](mathmodels/MathModelsMod/Images/MathModelsMod_gr_257.gif)
Figure 11.95 (a) Source and sink of unit strength.
The velocity potential and stream function are
, and
,
respectively. Solving for the
streamline
, we
start with
and obtain the equation
.
A straightforward calculation shows that points on the streamline
must satisfy the equation
,
which is the equation of a circle with center
at
that
passes through the points
. Several
streamlines are indicated in Figure 11.95(a).
Joukowski Transformation and Airfoils
Schwarz-Christoffel Transformation
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