Page 157 - 48Fundamentals of Compressible Fluid Mechanics
P. 157

The gas flow throw a long tube has a applicability in situations which occurs in a
         relatively long distance and where heat transfer is relatively rapid so that the tem-
         perature can be treated, for engineering purposes, as a constant. This model is  To put discussion when the
                                                                                  “relatively fast” means.
         applicable when a natural gas (or other gases) flows for a large distance. Such sit-
         uations are common in large cities in U.S.A. where natural gas is used for heating.
         It is more predominate (more applicable) in situations where the gas is pumped for
         a length of kilometers.
                The high speed of the gas is obtained or explained by the combination of
         heat transfer and the friction to the flow. For a long pipe, the pressure difference
         reduces the density of the gas. For instance, in a perfect gas, the density is inverse
         of the pressure (it has to be kept in mind that the gas undergoes a isothermal
         process.). To maintain conservation of mass, the velocity increases inversely to
         the pressure. At critical point the velocity reaches the speed of sound at the exit
                                       1
         and hence the flow will be chocked .
         8.1   The Control Volume Analysis/Governing equations

         Figure 8.1 describes the flow of gas from the left to the right. The heat transfer up
         stream (or down stream) is assumed to be negligible. Hence, the energy equation
         can be written as following:



                                                                             (8.1)





           1 This explanation is not correct as it will shown later on. Close to the critical point (about,    , the


         heat transfer, is relatively high and the isothermal flow model is not valid anymore. Therefore, the study
         of the isothermal flow above this point is academic discussion only.
                                           119
   152   153   154   155   156   157   158   159   160   161   162