Page 135 - Aerodynamics for Engineering Students
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1 18  Aerodynamics for Engineering Students

                   3.3.4  Solid boundaries and image systems
                   The  fact  that  the  flow  is  always  along  a  streamline and  not  through  it  has  an
                   important fundamental consequence. This is that  a  streamline of  an inviscid flow
                   can  be  replaced  by  a  solid  boundary  of  the  same  shape  without  affecting the
                   remainder of the flow pattern.  If, as often is the case, a streamline forms a closed
                   curve that separates the flow pattern into two separate streams, one inside and one
                   outside, then a solid body can replace the closed curve and the flow made outside
                   without altering the shape of the flow (Fig. 3.12a). To represent the flow in the region
                   of a contour or body it is only necessary to replace the contour by a similarly shaped
                   streamline. The following sections contain examples of simple flows which provide
                   continuous streamlines in the shapes of circles and aerofoils, and these emerge as
                   consequences of the flow combinations chosen.
                     When arbitrary contours and their adjacent flows have to be replaced by identical
                   flows containing similarly shaped streamlines, image systems have to be placed within
                   the contour that are the reflections of the external flow system in the solid streamline.
                     Figure 3.12b shows the simple case of a source A placed a short distance from an
                   infinite plane wall. The effect of the solid boundary on the flow from the source is
                   exactly represented by considering the effect of the image source A' reflected in the
                   wall. The source pair has a long straight streamline, i.e. the vertical axis of symmetry,
                   that separates the flows from the two sources and that may be replaced by a solid
                   boundary without affecting the flow.






































                   Fig. 3.12  Image systems
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