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CONVECTION HEAT TRANSFER
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                        the solid wall are one-dimensional with two nodes if linear elements are used. The pressure
                        may be averaged over each one-dimensional element to calculate the average pressure over
                        the boundary element. If this average pressure is multiplied by the length of the element,
                        the normal pressure acting on the boundary element is obtained. If the pressure force is
                        multiplied by the direction cosine in the flow direction, we obtain the local pressure drag
                        force in the flow direction. Integration of these forces over the solid boundary gives the
                        drag force due to the pressure D p .
                           The viscous drag force D f is calculated by integrating the viscous traction in the flow
                        direction, over the surface area. The relation for the total drag force in the x 1 direction may
                        be written for a two-dimensional case as

                                                =                                          (7.186)
                                             D x 1   [(−p + τ 11 )n 1 + τ 12 n 2 ]dA s
                                                    A s
                        where n 1 and n 2 are components of the surface normal n as shown in Figure 7.15.


                        7.8.3 Stream function

                        In most fluid dynamics and convection heat transfer problems, it is often easier to understand
                        the flow results if the streamlines are plotted. In order to plot these streamlines, or flow
                        pattern, it is first necessary to calculate the stream function values at the nodes. The lines
                        with constant stream function values, are referred to as streamlines. The stream function is
                        defined by the following relationships:

                                                             ∂ψ
                                                        u 1 =
                                                             ∂x 2
                                                              ∂ψ
                                                        u 2 =−                             (7.187)
                                                              ∂x 1
                        where ψ is the stream function. If we differentiate the first relation with respect to x 2 and
                        the second with respect to x 1 and then sum, we get the differential equation for the stream


                                                           n

                                                                        A s





                                             u a





                                    Figure 7.15 Normal gradient of velocity close to the wall
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