![]()
![]()
for
11.10 Image of a Fluid Flow
We have already examined several
two-dimensional fluid flows and have discovered that the image of a
flow under a conformal transformation is a flow. The
conformal mapping
, which
is obtained by using the Schwarz-Christoffel formula, (see Section
11.9), allows us to find the streamlines for flows in domains in
the w plane that are bounded by
straight-line segments.
The first technique is finding the image of a
fluid flowing horizontally from left to right across the upper half
plane
. The
image of the streamline
is
a streamline given by the parametric equations
and is oriented in the positive sense
(counterclockwise). The streamline
for
is
considered to be the boundary wall for a containing vessel for the
fluid flow.
Example 11.29. 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/FluidFlowImageMod_gr_12.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_12.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/FluidFlowImageMod_gr_18.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_18.gif)
Integrate and get
![[Graphics:Images/FluidFlowImageMod_gr_19.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_19.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/FluidFlowImageMod_gr_24.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_24.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).
Extra Example
1. Use Figure 11.88 to find the flow over the
vertical segment from
.
![[Graphics:Images/FluidFlowImageMod_gr_60.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_60.gif)
Figure 11.88 Flow over the vertical segment from.
Solution. Set
. In
the w-plane
,
and the exterior angles are
, and
the formula for the derivative
is
![[Graphics:Images/FluidFlowImageMod_gr_66.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_66.gif)
Integrate and get
![[Graphics:Images/FluidFlowImageMod_gr_67.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_67.gif)
Solve for the coefficients A and B and obtain
![]()
Extra Example 2. Use Figure 11.89 to find the flow around an infinitely long rectangular barrier.
![[Graphics:Images/FluidFlowImageMod_gr_78.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_78.gif)
Figure 11.89 Flow around an infinitely long rectangular barrier.
Solution. Set
. In
the w-plane
,
and the exterior angles are
, and
the formula for the derivative
is
![[Graphics:Images/FluidFlowImageMod_gr_83.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_83.gif)
Integrate and get
Solve for the coefficients
and
and obtain
![]()
Extra Example 3. Use Figure 11.90 to find the flow around
![[Graphics:Images/FluidFlowImageMod_gr_96.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_96.gif)
Figure 11.90 (a) Flow around one inclined segment in the upper half-plane.(b) Flow around two inclined segments forming a "V" in the plane.
Solution. Set
. In
the w-plane
,
and the exterior angles are
, and
the formula for the derivative
is
![[Graphics:Images/FluidFlowImageMod_gr_101.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_101.gif)
Integrate and get
![[Graphics:Images/FluidFlowImageMod_gr_102.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_102.gif)
Solve for the coefficients A and B and obtain
![]()
Extra Example 4. Use Figure 11.91 to find the flow over a dam.
![[Graphics:Images/FluidFlowImageMod_gr_115.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_115.gif)
Figure 11.91 Flow over a dam.
Solution. Set
. In
the w-plane
,
and the exterior angles are
, and
the formula for the derivative
is
![[Graphics:Images/FluidFlowImageMod_gr_120.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_120.gif)
Integrate and get
![[Graphics:Images/FluidFlowImageMod_gr_121.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_121.gif)
Solve for the coefficients A and B and obtain
![]()
Extra Example 5. Use Figure 11.92 to find the flow around
![[Graphics:Images/FluidFlowImageMod_gr_131.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_131.gif)
Figure 11.92 (a) Flow up an inclined step (b) Flow around a pointed object.
Solution. Set
. In
the w-plane
,
and the exterior angles are
, and
the formula for the derivative
is
![[Graphics:Images/FluidFlowImageMod_gr_136.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_136.gif)
Integrate and get
![[Graphics:Images/FluidFlowImageMod_gr_137.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_137.gif)
Solve for the coefficients A and B and obtain
![[Graphics:Images/FluidFlowImageMod_gr_138.gif]](fluidflowimage/FluidFlowImageMod/Images/FluidFlowImageMod_gr_138.gif)
Joukowski Transformation and Airfoils
Schwarz-Christoffel Transformation
Download This Mathematica Notebook
The Next Module is
Return to the Complex Analysis Modules
Return to the Complex Analysis Project