Page 262 - 48Fundamentals of Compressible Fluid Mechanics
P. 262

224                                       CHAPTER 13. OBLIQUE-SHOCK
                                            13.4.5   Flow in a Semi–2D Shape

                                            The discussion so far was about the straight infinite long wedge 20  which is
                                            a “pure” 2–D configuration.  Clearly, for any finite length of the wedge, the
                                            analysis needs to account for edge effects.  The end of the wedge must
                                            have a different configuration (see Figure 13.10).  Yet, the analysis for mid-
                                            dle section produces close results to reality (because symmetry).  The sec-
                                            tion where the current analysis is close to reality can be estimated from a
                                            dimensional analysis for the required accuracy or by a numerical method.
                                            The dimensional analysis shows that
                                            only doted area to be area where cur-  flow direction             no shock
                                            rent solution can be assumed as cor-       intermidiate analysis
                                                                                            range
                                                21
                                            rect .   In spite of the small area               normal analysis {
                                                                                                 range
                                                                                                      {
                                            were the current solution can be as-  no shock       { {
                                            sumed, this solution is also act as “re-    {
                                            ality check” to any numerical analysis.
                                            The analysis also provides additional
                                            value of the expected range.
                                                 Another geometry that can be
                                            considered as two dimensional is the
                                            cone (some referred to as Taylor–                         2-D oblique shock
                                                                                                      on both sides
                                            Maccoll flow). Eventhough, the cone          edge analysis
                                            is a three dimensional problem, the            range
                                            symmetrical nature of the cone cre-
                                            ates a semi–2D problem. In this case  Fig. 13.10: Schematic of finite wedge with zero
                                            there are no edge effects and the ge-        angle of attack
                                            ometry dictates slightly different re-
                                            sults. The mathematics is much more complicated but there are three solutions.
                                            As before, the first solution is thermodynamical unstable. Experimental and ana-
                                            lytical work shows that the weak solution is the stable solution and a discussion is
                                            provided in the appendix of this chapter. As oppose to the weak shock, the strong
                                            shock is unstable, at least, for steady state and no know experiments showing that
                                            it exist can be found the literature. All the literature, known to this author, reports
                                            that only a weak shock is possible.

                                            13.4.6   Small  “Weak Oblique shock”

                                            This topic has interest mostly from academic point of view. It is recommend to
                                            skip this issue and devote the time to other issues. This author, is not aware of a
                                              20 Even finite wedge with limiting wall can be considered as example for this discussion if the B.L. is
                                            neglected.
                                              21 At this stage dimensional analysis is not competed. This author is not aware of any such analysis
                                            in literature. The common approach is to carry numerical analysis. In spite recent trends, for most
                                            engineering application, simple tool are sufficient for limit accuracy. In additionally, the numerical works
                                            require many times a “reality check.”
   257   258   259   260   261   262   263   264   265   266   267