Page 28 - 48Fundamentals of Compressible Fluid Mechanics
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xxviii                                                       CONTENTS
                                                        11
                                            demonstrated .
                                                     The book is organized into several chapters which, as a traditional text-
                                            book, deals with a basic introduction of thermodynamics concepts (under construc-
                                            tion). The second chapter deals with speed of sound. The third chapter provides
                                            the first example of choked flow (isentropic flow in a variable area). The fourth
                                            chapter deals with a simple case of discontinuity (a simple shock wave in a noz-
                                            zle). The next chapter is dealing with isothermal flow with and without external
                                            forces (the moving of the choking point), again under construction. The next three
                                                                                                            12
                                            chapters are dealing with three models of choked flow: Isothermal flow , Fanno
                                            flow and Rayleigh flow. First, the Isothermal flow is introduced because of the rel-
                                            ative ease of the analytical treatment. Isothermal flow provides useful tools for the
                                            pipe systems design. These chapters are presented almost independently. Every
                                            chapter can be “ripped” out and printed independently. The topics of filling and
                                            evacuating of gaseous chambers are presented, normally missed from traditional
                                            textbooks. There are two advanced topics which included here: oblique shock
                                            wave, and properties change effects (ideal gases and real gases) (under construc-
                                            tion). In the oblique shock, for the first time analytical solution is presented, which
                                            is excellent tool to explain the strong, weak and unrealistic shocks. The chapter on
                                            one-dimensional unsteady state, is currently under construction.
                                                     The last chapter deals with the computer program, Gas Dynamics Cal-
                                            culator (CDC-POTTO). The program design and how to use the program are de-
                                            scribed (briefly).
                                                     Discussions on the flow around bodies (wing, etc), and Prandtl–Meyer
                                            expansion will be included only after the gamma version unless someone will pro-
                                            vide discussion(s) (a skeleton) on these topics.
                                                     It is hoped that this book will serve the purposes that was envisioned
                                            for the book. It is further hoped that others will contribute to this book and find
                                            additional use for this book and enclosed software.






















                                              11 If you have better and different examples or presentations you are welcome to submit them.
                                              12 It is suggested to referred to this model as Shapiro flow
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