Page 78 - 48Fundamentals of Compressible Fluid Mechanics
P. 78

40                       CHAPTER 4. ISENTROPIC VARIABLE AREA FLOW

                                            noted by the subscript “
 .”
                                                   First, the stagnation tempera-
                                            ture is calculated. The energy conser-
                                            vation can be written as

                                                                                                                (4.1)




                                             Perfect gas is an ideal gas with a constant heat capacity,    . For perfect gas


                                            equation (4.1) is simplified into
                                                                                                                (4.2)




                                             Again it common to denote 
  as the stagnation temperature. Recalling from


                                            thermodynamic the relationship for perfect gas
                                                                                                                (4.3)

                                                                    than the thermodynamics relationship obtains the form



                                             and denoting
                                                                                                                (4.4)


                                                                                                         yield





                                                         is a specific constant. Dividing equation (4.2) by
                                             and where
                                                                                                                (4.5)





                                                                                  equation (4.5) changes into


                                             Now, substituting    
 or
                                                                                                                (4.6)








                                             Utilizing the definition of  by equation (4.4) and inserting it into equation (4.6)



                                            yields
                                                                                                                (4.7)







                                                   It very useful to convert equation (4.6) into a dimensionless form and de-


                                            note Mach number as the ratio of velocity to speed of sound as
                                                                                                                (4.8)

                                             Inserting the definition of Mach number, (4.8) into equation (4.7) reads


                                                                                                                (4.9)
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