Page 495 - Modelling in Transport Phenomena A Conceptual Approach
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11.1.  UNSTEADY LAMINAR FLOW IN A TUBE                             475

           Substitution  of  Eqs.  (11.1-1)  and  (11.1-3)  into  Eq. (11.1-7)  and  noting  that
           dv,/dz  = 0 gives
                                 dv,     dP   p  a
                               Pdt=-- +;z(r%)+pg                            (1 1 .l-8)
                                         dz
           The modified pressure is defined by

                                         P=P-pgz                            (1 1.1-9)
           so that
                                        dP
                                        _-                                 (1 1.1-10)
                                              dP
                                            --
                                         dz   dz   - PS
           Substitution of  Eq.  (11.1-10) into Eq.  (11.1-8) yields
                                   av,
                                           a
                                 p=-;z(r%)=-z             dP
                                         p
                                                                           (1 1.1-11)
                                 \        "         4  -
                                         f (V)          f (4
           Note that while the right-side of  Eq.  (11.1-11) is a function of  z only, the left-side
           is dependent on r and t. This is possible if and only if both sides of  Eq.  (11.1-11)
           are equal to a constant, say A.  Hence,

                                 dP  -A     *      A=   Po - PL            (11 .l-12)
                                 dz                       L
           where Po and PL are the values of P at z = 0 and I = L, respectively. Substitution
           of  Eq.  (11.1-12) into Eq.  (11.1-11) gives the governing equation for velocity as


                                                                           (1 1 .l-13)

           The initial and the boundary conditions associated with Eq. (11.1-13) are

                                at  t = 0   v, =O     for all r           (11.1-14)

                               at  r=O      -- - o     for t 2 o           (1 1 .l-15)
                                            "2
                                            dr
                                atr=R        vz=O     fort20              (11.1-16)

           11.1.1  Exact Solution

           Introduction of  the following dimensionless quantities

                                                                          (1 1.1-17)
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