Page 45 - 48Fundamentals of Compressible Fluid Mechanics
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1.3. HISTORICAL BACKGROUND                                            7
                                      19
         conditions to a more general form .
                  Here, the second law has been around for over 40 years and yet the
         significance of it was not was well established. Thus, it took over 50 years for
                                                                              20
         Prandtl to arrive at and to demonstrate that the shock has only one direction .
         Today this equation/condition is known as Prandtl’s equation or condition (1908). In
         fact Prandtl is the one who introduced the name of Rankine-Hugoniot’s conditions
         not aware of the earlier developments of this condition. Theodor Meyer (Prandtl’s
         student) derived the conditions for oblique shock in 1908 21  as a byproduct of the
         expansion work.

                  It was probably later
         that Stodola (Fanno’s adviser)
         realized that the shock is the in-
         tersection of the Fanno line with
         the Rayleigh line. Yet, the su-
         personic branch is missing from
         his understanding (see Figure
         1.1). In fact, Stodola suggested
         the graphical solution utilizing
         the Fanno line.

                  The fact that the
         conditions and direction were
         known did not bring the solu-
         tion to the equations. The “last
         nail” of understanding was put
         by Landau, a Jewish scientist
         who worked in Moscow Univer-
         sity in the 1960’s during the
                                      Fig. 1.1: The shock as connection of Fanno and
         Communist regimes. A solution
                                             Rayleigh lines after Stodola, Steam and Gas
         was found by Landau & Lifshitz      Turbine
         and expanded by Kolosnitsyn &
         Stanyukovich (1984).                                                     to be add to oblique shock
                                                                                  chapter.
                  Since early of the 1950 the relationship between the the oblique shock
         deflection angle and shock angle and Mach number was described as not possible
         to obtained. There were up recently (version 0.3 of this book) several equations
         that tied various properties/quantities. The first analytical solution connecting the
         angles with upstream Mach number was published in this book version 0.3. The
         probable reason that analytical solution was not published because the claim in the




          19 To add discussion about the general relationships.
          20 Some view the work of G. I. Taylor from England as the proof (of course utilizing the second law)
          21 Theodor Meyer in Mitteil. ¨ub. Forsch-Arb. Berlin, 1908, No. 62, page 62.
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