Page 88 - Mechanical Engineers' Handbook (Volume 4)
P. 88

11 Viscous Fluid Flow in Ducts  77

                           velocity profile also changes and becomes adjusted to a fixed shape. When these have reached
                           constant conditions, the flow is called fully developed flow.
                              The momentum equation for a pipe of diameter D gives the pressure gradient as
                                                   dp   4        d        dV
                                                               V  2      V
                                                          0
                                                   dx   D        dx       dx
                           which shows that a pressure gradient overcomes wall shear and increases momentum of the
                           fluid either as a result of changing the shape of the velocity profile (d /dx) or by changing
                           the mean velocity along the pipe (dV/dx is not zero for gas flows).
                              For fully developed incompressible flow
                                                          dp  
p   4  0

                                                          dx   L    D
                           and a pressure drop simply overcomes wall shear.
                              For developing flow in the entrance,     1 initially and increases to a constant value
                           downstream. Thus, the pressure gradient overcomes wall shear and also increases the flow
                           momentum according to

                                                        dp  4        d
                                                              0     V  2
                                                        dx   D       dx
                                                   4
                           For fully developed flow,     ⁄3 for laminar flow and   
 1.03 for turbulent flow in round
                           pipes.
                              For compressible gas flow beyond the entrance, the velocity profile becomes essentially
                           fixed in shape, but the velocity changes because of thermodynamic effects that change the
                           density. Thus, the pressure gradient is
                                                        dp  4  0     dV
                                                                   V
                                                        dx   D       dx
                           Here   is essentially constant but dV/dx may be significant.


            11.1  Fully Developed Incompressible Flow
                                                          2
                           The pressure drop is 
p   (ƒL/D)( V /2) Pa, where ƒ is the Darcy friction factor. The
                                                                            2
                           Fanning friction factor ƒ    ƒ/4 and then 
p   (4ƒ /D)( V /2), and the head loss from
                           pipe friction is
                                                  
p   ƒ     V  2   (4ƒ )    V  2
                                                          L
                                                                       L
                                              h                               m
                                               ƒ
                                                          D 2g         D 2g
                              The shear stress varies linearly with radial position,     (
p/L)(r/2), so that the wall
                                                                              2
                                                                                       2
                           shear is     (
p/L)(D/4), which may then be written     ƒ V /8   ƒ  V /2.
                                  0                                    0
                              A shear velocity is defined as v       /     V ƒ/8    V ƒ /2  and is used as a
                                                               0
                           normalizing parameter.
                              For noncircular ducts the diameter D is replaced by the hydraulic or equivalent diameter
                           D   4.4/P, where A is the flow cross section and P is the wetted perimeter. Thus, an
                            h
                           annulus between pipes of diameter D and D , D being larger, the hydraulic diameter is D 2
                                                              2
                                                        1
                                                                 1
                             D .
                              1
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