Page 87 - Aerodynamics for Engineering Students
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70  Aerodynamics for Engineering Students

                                    Yt







                                       I     P(x, y)





                  Fig. 2.11

                  Thus
                                                 4' = q: + 4:
                   and the direction of q relative to the radius vector is given by

                                                 p = tan-  1%
                                                          4n

                   Fluid acceleration
                   The equation of acceleration of a fluid mass is rather different from that of a vehicle,
                   for example, and a note on fluid acceleration follows. Let a fluid particle move from
                   P  to  Q in time St in a  two-dimensional flow (Fig. 2.11). At the point P(x, y) the
                   velocity  components  are  u  and  v.  At  the  adjacent  point  Q(x+ Sx, y+ by)  the
                   velocity components are u + 61.4 and v + Sv, i.e. in general the velocity component
                   has changed in each direction by an increment  Su or Sv. This incremental change is the
                   result of a spatial displacement, and as u and v are functions of x  and y the velocity
                   components at Q are
                                     au     au                     aV     av
                                        Sx
                          u + Su = u + - + -by     and  v + Sv = v + - SX + - Sy      (2.34)
                                     ax     ay                     ax     ay
                   The component of acceleration in the On direction is thus
                                         d(u+Su)  au  dudx  audy
                                                  --+--+--
                                                  -
                                            dt      at  dxdt  aydt
                                                    au    au    au
                                                  =-+u-+v-                            (2.35)
                                                    at    ax    ay
                   and in the Oy direction
                                           d(v+ Sv)  au    dv    dv                   (2.36)
                                                   -_ +u-+v-
                                              dt   -  at   ax    ay
                   The change in other flow variables, such as pressure, between points P and Q may be dealt
                   with in a similar way. Thus, if the pressure takes the value p at P, at Q it takes the value

                                                       aP     aP
                                           p + sp = p + -6x  + -6y                    (2.37)
                                                       ax     ay
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