Page 71 - Air pollution and greenhouse gases from basic concepts to engineering applications for air emission control
P. 71

2.1 Gas Kinetics                                                45

              The viscosities at different reference temperatures can be found in the handbook
            of CRC [5]; and some examples are listed Table 2.2. For temperatures between
            0 < T < 555 K, the Sutherland’s constants and reference temperatures for some
            gases are listed. The maximum error is 10 %.



            2.2 Gas Fluid Dynamics

            2.2.1 Reynolds Number


            Reynolds number of a fluid quantifies the relative importance of inertial forces (qu)
            and viscous forces (μ/L) for a flow. Mathematically, it is described by

                                          quD    4 _ m
                                      Re ¼     ¼                         ð2:71Þ
                                            l    lpD

            where u ¼ magnitude of the mean fluid velocity in m/s, D ¼ characteristic length in
                                                   2
            m, l ¼ dynamic viscosity of the fluid in N:s=m Þ or Pa.s, q ¼ density of the fluid
                                             ð
                  3
            in kg/m , and _ m is the mass flow rate of the fluid.
              The characteristic length depends on the flow condition, internal or external, and
            the cross section of the pipe for internal flow. For flow in a pipe, it is the hydraulic
            diameter of the pipe, and for flow over a body, the characteristic length is usually
            the length of the body. The flow is likely laminar if Re < 2,000 and turbulent for
            Re > 4,000 for either internal or external flows. In a boundary layer analysis
            (Sect. 2.2.3), the characteristic length is the distance measured from the leading
            edge where the boundary layer starts to develop.



            2.2.2 Bernoulli’s Equation


            Bernoulli’s equation is important to air emission analysis too. It is derived from the
            basic concept of conservation of mass and conservation of energy. Very briefly,
            consider a streamline of a moving fluid without heat transfer; Bernoulli’s equation
            describes the relationship between the static pressure of the fluid, fluid velocity, and
            the elevation for a steady flow,

                                  v 2  Z  DP
                                    þ      þ gz ¼ constant               ð2:72Þ
                                  2      q
            where v is the local velocity on the streamline (m/s), P is the absolute static pressure
                                                3
                   2
            (Pa; N/m ), q is the density of the fluid (kg/m ), g is gravitational acceleration (9.81
               2
            m/s ) and z is the elevation (m).
   66   67   68   69   70   71   72   73   74   75   76