Page 240 - 48Fundamentals of Compressible Fluid Mechanics
P. 240

202CHAPTER 12. EVACUATING/FILING CHAMBERS UNDER EXTERNAL VOLUME CONTROL

                                             Now substituting to the “preferred” variable





                                                                                                               (12.9)

                                                                                     #% &

                                                                B


                                                                                             L

                                                                 B


                                                                           >

                                                                                             L
                                             The analytical solution is applicable only in the case which the flow is choked
                                                                                             L
                                                                                             L

                                                              E #%'&  >
                                            thorough all the process. The solution is applicable to indirect connection. This
                                                                                                  >*

                                                                                             L
                                                                                             L

                                            happen when vacuum is applied outside the tube (a technique used in die casting
                                                                    >
                                            and injection molding to improve quality by reducing porosity.). In case when the

                                            flow chockless a numerical integration needed to be performed. In the literature, to


                                            create a direct function equation (12.4) is transformed into


                                                                                                              (12.10)
                                                                            B

                                                                             B
                                                                                     <

                                             with the initial condition of       E  >*
                                                                        : E #% &  >
                                                                                       >


                                                                  >
                                                                                                              (12.11)

                                                                  >*




                                                   The analytical solution also can be approximated by a simpler equation as

                                                                                                              (12.12)
                                                                                  #%'&

                                             The results for numerical evaluation in the case when cylinder is initially at an
                                                                        >  *
                                            atmospheric pressure and outside tube is also at atmospheric pressure are pre-
                                                                              E
                                            sented in figure 12.2. In this case only some part of the flow is choked (the later
                                            part). The results of a choked case are presented in figure 12.3 in which outside
                                            tube condition is in vacuum. These figures 12.2 and 12.3 demonstrate the impor-
                                                                                 the pressure increases significantly and

                                            verse versa.      B  B  . When #%'&   B
                                            tance of the ratio of #%'&
                                                   Thus, the question remains how the time ratio can be transfered to param-
                                                                         B
                                            eters that can the engineer can design in the system.
                                                                                      can be expressed as           @
                                                   Denoting the area that creates the ratio #%'&

                                                                                        B
                                                                                         B
                                                                                                              (12.13)
                                                                                                as the critical area,
                                            provides the needed tool. Thus the exit area,
                                                                        can be expressed as
                                                                                  @
                                                                                @


                                             The actual times ratio #%'&

                                                                 B

                                                                  B L
                                                                     L

                                                                     L
                                                                                                              (12.14)







                                                                   ?PO
                                                                              ?PO
                                                                                      ?AO
                                                                                L
                                                                                        L
                                                                      L
                                                                            N
                                                                                     N
                                                                  N
                                                                              @ L @ L
                                                                   @ L
                                                                          *
                                                                 *
                                                                                    *
                                                                  * L * L * L
                                                                      L
                                                                                L
                                                                                        L
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