Page 83 - 48Fundamentals of Compressible Fluid Mechanics
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4.2. ISENTROPIC CONVERGING-DIVERGING FLOW IN CROSS SECTION 45

                                         from the mass balance equation (4.26) and
         utilizing it in equation (4.28) reads
         Obtaining an expression for

                                                                           (4.30)





                                                      , can be replaced by the static



                      yields
         Rearranging equation (4.30) so that the density,

         pressure,

                                                                           (4.31)






















                                 and substitute the speed of sound into equation (4.31)

         to obtain




         Recalling that
                                                                           (4.32)






                                     &


         Or in a dimensionless form           (
                                                                           (4.33)





         Equation (4.33) is a differential equation for the pressure as a function of the cross

         section area. It is convenient to rearrange equation (4.33) to obtain a variables

         separation form of
                                                                           (4.34)









         4.2.1.1 The pressure relationship to Mach number
         Before going further in the mathematical derivation it is worth in looking at the
                                                        is always positive (because

                                                                             can
                                                 and Mach number. The meaning of

         physical meaning equation (4.34). The term

         the sign change for the pressure differential is that the pressure can increase or
         all the three terms can be only positive). Now, it can be observed that
         be positive or negative deepening on the
         decrease. It can be observed that the critical Mach number is one. If the Mach
                                                              . If Mach number is

                                         has opposite sign of
         number is larger than one than
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