Page 252 - 48Fundamentals of Compressible Fluid Mechanics
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214                                       CHAPTER 13. OBLIQUE-SHOCK

                                             and where the definitions of  and  are

                                                                                                              (13.29)
                                                                       "
                                                                            ,	 E ,
                                             and                                  "

                                                                                                              (13.30)


                                                                                  )
                                                                     "  ", ,	 E , E ,
                                             Only three roots can exist for Mach angle,  . From mathematical point of view, if
                                                                                 9
                                                                                                          all the roots
                                                                                          .
                                                                                                          all the roots

                                                  one root is real and two roots are complex. For the case
                                            are real and unequal.
                                                                                    .
                                            are real and at least two are identical. In the last case where
                                                 The physical meaning of the above analysis demonstrates that in the range


                                                                                                            10
                                            occurs when no shock angle can be found so that the shock normal component is
                                                         no solution exist because no imaginary solution can exist .
                                            where
                                            reduced to be subsonic and yet be parallel to inclination angle.
                                                                                              the solution has physical


                                                                                         has to be examined in the light
                                                 Furthermore, only in some cases when
                                            of other issues to determine the validity of the solution.
                                            meaning. Hence, the solution in the case of
                                                              the three unique roots are reduced to two roots at least for

                                                                                          11
                                            steady state because the thermodynamics dictation . Physically, it can be shown

                                                 When
                                            that the first solution(13.23), referred sometimes as thermodynamically unstable
                                            root which also related to decrease in entropy, is “unrealistic.” Therefore, the first

                                            solution dose not occur in reality, at least, in steady state situations. This root has
                                                                                            12
                                            only a mathematical meaning for steady state analysis .
                                                 These two roots represents two different situations. One, for the second root,
                                            the shock wave keeps the flow almost all the time as supersonic flow and it refereed
                                            to as the weak solution (there is a small branch (section) that the flow is subsonic).
                                            Two, the third root always turns the flow into subsonic and it refereed to a strong
                                            solution. It should be noted that this case is where entropy increases in the largest
                                            amount.
                                                 In summary, if there was hand which moves the shock angle starting with
                                            the deflection angle, reach the first angle that satisfies the boundary condition,
                                            however, this situation is unstable and shock angle will jump to the second angle
                                            (root). If additional “push” is given, for example by additional boundary conditions,
                                              10 A call for suggestions, should explanation about complex numbers and imaginary numbers should
                                            be included. Maybe insert example where imaginary solution results in no physical solution.
                                              11 This situation is somewhat similar to a cubical body rotation. The cubical body has three symmetri-
                                            cal axises which the body can rotate around. However, the body will freely rotate only around two axis
                                            with small and large moments of inertia. The body rotation is unstable around the middle axes. The
                                            reader simply can try it.
                                              12 There is no experimental evidence, that this author found, showing that it is totally impossible.
                                            Though, those who are dealing with rapid transient situations should be aware that this angle of the
                                            oblique shock can exist. The shock initially for a very brief time will transient in it and will jump from this
                                            angle to the thermodynamically stable angles.
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