Module

for

Image of a Fluid Flow

 

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 [Graphics:Images/FluidFlowImageMod_gr_1.gif],  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  [Graphics:Images/FluidFlowImageMod_gr_2.gif].  The image of the streamline  [Graphics:Images/FluidFlowImageMod_gr_3.gif]  is a streamline given by the parametric equations

            [Graphics:Images/FluidFlowImageMod_gr_4.gif]  

and is oriented in the positive sense (counterclockwise).  The streamline  [Graphics:Images/FluidFlowImageMod_gr_5.gif]  for  [Graphics:Images/FluidFlowImageMod_gr_6.gif]  is considered to be the boundary wall for a containing vessel for the fluid flow.

 

 

Example 11.29.  Show that the mapping  [Graphics:Images/FluidFlowImageMod_gr_7.gif]  maps the upper half plane [Graphics:Images/FluidFlowImageMod_gr_8.gif]  onto the domain in the w-plane that lies above the boundary curve consisting of the rays  [Graphics:Images/FluidFlowImageMod_gr_9.gif] and the segment  [Graphics:Images/FluidFlowImageMod_gr_10.gif]   (see Figure 11.87).

[Graphics:Images/FluidFlowImageMod_gr_12.gif]

            Figure 11.87  (a) Flow over a step.                  (b) Flow around a blunt object.

Hint:  Set  [Graphics:Images/FluidFlowImageMod_gr_13.gif]  and   [Graphics:Images/FluidFlowImageMod_gr_14.gif].  In the w-plane [Graphics:Images/FluidFlowImageMod_gr_15.gif], and the exterior angles are  [Graphics:Images/FluidFlowImageMod_gr_16.gif],  and the formula for the derivative [Graphics:Images/FluidFlowImageMod_gr_17.gif] is  

            [Graphics:Images/FluidFlowImageMod_gr_18.gif]

Integrate and get  

            [Graphics:Images/FluidFlowImageMod_gr_19.gif]

Solve for the coefficients A and B and obtain

            [Graphics:Images/FluidFlowImageMod_gr_20.gif]

It maps the upper half-plane [Graphics:Images/FluidFlowImageMod_gr_21.gif]  onto the domain in the w plane that lies above the boundary curve consisting of the rays  [Graphics:Images/FluidFlowImageMod_gr_22.gif] and the segment  [Graphics:Images/FluidFlowImageMod_gr_23.gif].  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]

for  [Graphics:Images/FluidFlowImageMod_gr_25.gif].  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 [Graphics:Images/FluidFlowImageMod_gr_26.gif] 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).

Explore Solution 11.29.

 

Extra Example 1.  Use Figure 11.88 to find the flow over the vertical segment from [Graphics:Images/FluidFlowImageMod_gr_58.gif].

[Graphics:Images/FluidFlowImageMod_gr_60.gif]

            Figure 11.88  Flow over the vertical segment from [Graphics:Images/FluidFlowImageMod_gr_61.gif].

Solution.  Set  [Graphics:Images/FluidFlowImageMod_gr_62.gif].  In the w-plane [Graphics:Images/FluidFlowImageMod_gr_63.gif], and the exterior angles are  [Graphics:Images/FluidFlowImageMod_gr_64.gif],  and the formula for the derivative [Graphics:Images/FluidFlowImageMod_gr_65.gif] is  


            [Graphics:Images/FluidFlowImageMod_gr_66.gif]

Integrate and get  

            [Graphics:Images/FluidFlowImageMod_gr_67.gif]

Solve for the coefficients A and B and obtain

            [Graphics:Images/FluidFlowImageMod_gr_68.gif]

Explore Extra Solution 1.

 

Extra Example 2.  Use Figure 11.89 to find the flow around an infinitely long rectangular barrier.

[Graphics:Images/FluidFlowImageMod_gr_78.gif]

            Figure 11.89  Flow around an infinitely long rectangular barrier.

Solution.  Set  [Graphics:Images/FluidFlowImageMod_gr_79.gif].  In the w-plane [Graphics:Images/FluidFlowImageMod_gr_80.gif], and the exterior angles are  [Graphics:Images/FluidFlowImageMod_gr_81.gif],  and the formula for the derivative [Graphics:Images/FluidFlowImageMod_gr_82.gif] is  


            [Graphics:Images/FluidFlowImageMod_gr_83.gif]

Integrate and get  

            [Graphics:Images/FluidFlowImageMod_gr_84.gif]  

Solve for the coefficients [Graphics:Images/FluidFlowImageMod_gr_85.gif] and [Graphics:Images/FluidFlowImageMod_gr_86.gif] and obtain

            [Graphics:Images/FluidFlowImageMod_gr_87.gif]

Explore Extra Solution 2.

 

Extra Example 3.  Use Figure 11.90 to find the flow around

[Graphics: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  [Graphics:Images/FluidFlowImageMod_gr_97.gif].  In the w-plane [Graphics:Images/FluidFlowImageMod_gr_98.gif], and the exterior angles are  [Graphics:Images/FluidFlowImageMod_gr_99.gif],  and the formula for the derivative [Graphics:Images/FluidFlowImageMod_gr_100.gif] is  


            [Graphics:Images/FluidFlowImageMod_gr_101.gif]

Integrate and get  

            [Graphics:Images/FluidFlowImageMod_gr_102.gif]

Solve for the coefficients A and B and obtain

            [Graphics:Images/FluidFlowImageMod_gr_103.gif]

Explore Extra Solution 3.

 

Extra Example 4.  Use Figure 11.91 to find the flow over a dam.

[Graphics:Images/FluidFlowImageMod_gr_115.gif]

            Figure 11.91  Flow over a dam.

Solution.  Set  [Graphics:Images/FluidFlowImageMod_gr_116.gif].  In the w-plane [Graphics:Images/FluidFlowImageMod_gr_117.gif], and the exterior angles are  [Graphics:Images/FluidFlowImageMod_gr_118.gif],  and the formula for the derivative [Graphics:Images/FluidFlowImageMod_gr_119.gif] is  

            [Graphics:Images/FluidFlowImageMod_gr_120.gif]

Integrate and get  

            [Graphics:Images/FluidFlowImageMod_gr_121.gif]

Solve for the coefficients A and B and obtain

            [Graphics:Images/FluidFlowImageMod_gr_122.gif]

Explore Extra Solution 4.

 

Extra Example 5.  Use Figure 11.92 to find the flow around

[Graphics:Images/FluidFlowImageMod_gr_131.gif]

            Figure 11.92  (a) Flow up an inclined step                    (b) Flow around a pointed object.

Solution.  Set  [Graphics:Images/FluidFlowImageMod_gr_132.gif].  In the w-plane [Graphics:Images/FluidFlowImageMod_gr_133.gif], and the exterior angles are  [Graphics:Images/FluidFlowImageMod_gr_134.gif],  and the formula for the derivative [Graphics:Images/FluidFlowImageMod_gr_135.gif] is  


            [Graphics:Images/FluidFlowImageMod_gr_136.gif]

Integrate and get  

            [Graphics:Images/FluidFlowImageMod_gr_137.gif]

Solve for the coefficients A and B and obtain

            [Graphics:Images/FluidFlowImageMod_gr_138.gif]

Explore Extra Solution 5.

 

Library Research Experience for Undergraduates

Ideal Fluid Flow

Joukowski Transformation and Airfoils

Schwarz-Christoffel Transformation

 

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