Page 126 - 48Fundamentals of Compressible Fluid Mechanics
P. 126

88                                         CHAPTER 5. NORMAL SHOCK
                                            5.3.2   Moving Shock Into Stationary Medium

                                            5.3.2.1  General Velocities Issues

                                            When valve or membrane is suddenly opened a shock is created and propagate
                                            the downstream. With the exception of a close proximity to the valve, the shock is
                                            moving in a constant velocity (see Figure (5.8)). Converting the moving shock to a
                                            coordinates system that attached to the shock results in a stationary shock when
                                            the flow is moving to left. The “upstream” is on the right (see Figure (5.8)).




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                                                      (a) The reflective shock into            (b) The reflective shock into
                                                      close end pipe in stationary            close end pipe in moving co-
                                                      coordinates                             ordinates


                                                        Fig. 5.8: The reflective shock into close end pipe coordinates

                                                   Similar definitions of the right and the left side shock Mach numbers for are
                                            utilized. It has to be noticed that the “upstream” and “downstream” are the reverse
                                            from the previous case. The “upstream” Mach number is

                                                                                                               (5.59)


                                             The “downstream” Mach number is
                                                                                                               (5.60)






                                                   Note that in this case the stagnation temperature in stationary coordinate

                                            changes (as in the previous case) where the thermal energy (due to pressure dif-
                                            ference) is converted into velocity. The stagnation temperature (of moving coordi-
                                            nates) is
                                                                                                               (5.61)















                                             After similar rearrangement as in the previous case results in




                                                                                                               (5.62)
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