Page 280 - 48Fundamentals of Compressible Fluid Mechanics
P. 280

242                                       CHAPTER 13. OBLIQUE-SHOCK

                                            Example 13.14:
                                            The previous example give raise to another question the order of the deflection
                                            angles. Consider the same values as previous analysis, if oblique shock with first
                                                            and     or opposite order make a difference (     9 )? If not
                                            what order make bigger entropy production or pressure loss? (No general proof is
                                            with angle of 9
                                            needed).
                                              SOLUTION
                                            Waiting for the solution


                                            13.4.13    Optimization of Suction Section Design
                                            Under heavy construction please ignore
                                                 The question raises what is the optimum design for inlet suction unit. The
                                            are several considerations that have to be taken into account aside to supersonic
                                            flow which include for example the material strength consideration and operation
                                            factors.
                                                 The optimum deflection angle is a function of the Mach number range in with
                                            suction section is operated in. The are researchers that suggest that the numerical
                              is presentation of the ex-
                              perimental works is useful
                              here?  or present the nu- work with possibility to work the abrupt solution.
                              merical works?  Perhaps to
                              present the simplified model.
                                            13.5     Summary
                                            As normal shock, the oblique shock the upstream Mach number,  is always

                                            could be larger or smaller then 1. The perpendicular component of the downstream
                                                              is always smaller than 1. For given  and deflection angle,

                                            c there could be three solutions: the first one is the “impossible” solution in case

                                            Mach number,
                                            where D is negative two the weak shock, and three the strong shock. When D is

                                            greater than 1. However, not as the normal shock downstream Mach number,
                                            positive there no physical solution and only normal shock exist. When D is equal


                                            to zero, a spacial case is created for the weak and strong solution are equal (for
                                                                            , for large deflection angle, there is possibility
                                            of no two-dimensional solution resulting in a detached shock case.
                                            large deflection angle). When
                                            13.6     Appendix: Oblique Shock Stability Analysis

                                            The stability analysis is an
                                            analysis which answer the
                                            question what happen if for                           Unstable    Stable
                                            some reasons, the situation
                                            moves away from the ex-
                                            pected solution. If the an-
                                            swer turned out to be that  Fig. 13.21: Typical examples of of unstable and stable situ-
                                            situation will return to its       ations
   275   276   277   278   279   280   281   282   283   284   285