Page 127 - 48Fundamentals of Compressible Fluid Mechanics
P. 127

5.3. THE MOVING SHOCKS                                               89


                   Shock in A Suddenly Open Valve       Shock in A Suddenly Open Valve
                          k = 1 4, M ’ = 0.3                   k = 1 4, M ’ = 1.3
                               y                                   y
              1.75                                   4
                           M                                    M
                            x                                    x
                           M                        3.5         M
                            y                                    y
               1.5         T /T x                    3          T /T x
                                                                 y
                            y
                                                    2.5
              1.25
                                                     2
                                                    1.5
                1
                                                     1
                                                    0.5
              0.75
                0                     10             0      5     10     15     20
                          Number of Iteration                  Number of Iteration
             Wed Aug 23 17:20:59 2006             Wed Aug 23 17:46:15 2006
                  (a) The number of iterations to      (b) The number of iterations to

                                                       achieve the results for



                  achieve the results for
                The same question that was prominent in the previous case appears now.
         what will be the shock velocity for given upstream Mach number? The relationship
         again between the two sides is

                                                                           (5.63)
                                                      %



                                           theatrically equation (5.63) can be solved.



                                              %
                                             %
         It is common practice to solve this equation by numerical methods. One of such
         method is successive substitutions. This method is done by the following algorithm:
                   can be transformed to
         Since

                                        utilizing the tables or Potto–GDC
         (a) Assume that


         (c) Utilizing
         (b) Calculate the Mach number





                                          against the old one. If it satisfactory stop or
            calculate the new “improved”
            return to stage (b).

                                   
 ,
         (d) Check the new and improved
         
 
 and 
 
 . The results show that the convergence occurs very rapidly
                To illustrate the convergence of the procedure consider the case of
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