Page 210 - Bird R.B. Transport phenomena
P. 210

194  Chapter 6  Interphase Transport in Isothermal Systems

      in  which the Reynolds number is defined  by     6A.10  Determination of pipe diameter.  What  size of cir-
                                                       cular  pipe  is  needed  to produce a  flow  rate  of  250  firkins
                                              (6A.7-3)  per  fortnight when there is a pressure drop of 3 X 10  scru-
                                                                                                5
                                                       ples  per  square  barleycorn?  The  pipe  is  horizontal.  (The
      The  values  of  G, H, and К are given  as: 1
                                                       authors are indebted  to Professor  R. S. Kirk  of  the Univer-
                                                       sity  of  Massachusetts,  who  introduced  them  to  these
                      H       К
                                                       units.)
      0.00  4.000   0.400   1.000                      6B.1  Effect  of  error in  friction  factor  calculations.  In a
      0.05  3.747   0.293   0.7419                     calculation using  the Blasius  formula  for  turbulent flow  in
      0.10  3.736   0.239   0.7161                     pipes, the Reynolds number used  was  too low  by  4%. Cal-
      0.15  3.738   0.208   0.7021                     culate the resulting error in the friction  factor.
      0.20  3.746   0.186   0.6930                     Answer: Too high by  1 %
      0.30  3.771   0.154   0.6820
      0.40  3.801   0.131   0.6759                     6B.2  Friction factor for flow along a flat plate. 2
      0.50  3.833   0.111   0.6719                     (a)  An  expression  for  the drag  force  on a flat  plate, wetted
      0.60  3.866   0.093   0.6695                     on  both sides, is given  in Eq. 4.4-30. This equation was  de-
      0.70  3.900   0.076   0.6681                     rived  by  using  laminar  boundary  layer  theory  and  is
      0.80  3.933   0.060   0.6672                     known  to be  in  good  agreement  with  experimental  data.
      0.90  3.967   0.046   0.6668                     Define  a  friction  factor  and  Reynolds  number, and obtain
                                                       the / versus
                                                                Re relation.
      1.00  4.000   0.031   0.6667
                                                       (b)  For turbulent flow, an approximate boundary layer treat-
                                                       ment based on the 1/7  power velocity distribution gives
      Equation  6A.7-2 is based  on Problem 5C.2 and reproduces                       y5
      the  experimental  data  within  about  3%  up  to  Reynolds  F  = 0.072pviWL(Lv p/fjir  (6B.2-1)
                                                                                  x
                                                                   k
      numbers  of  20,000.                             When  0.072 is replaced by  0.074, this relation describes  the
                                                                                            5
      (a)  Verify  that Eqs.  6A.7-1 and  2 are equivalent  to the re-  drag  force within experimental error for  5  X 10  < Lv^pZ/x
                                                               7
      sults given  in §2.4.                            <  2  X  10 .  Express  the corresponding  friction  factor  as  a
      (b)  An annular duct is formed  from cylindrical  surfaces  of  function  of the Reynolds number.
      diameters  6  in. and  15  in.  It is  desired  to pump  water  at  6B.3  Friction  factor  for  laminar  flow  in  a  slit.  Use  the
      60°F at a rate of  1500 cu ft per second. How much pressure  results  of Problem 2B.3 to show  that for the laminar flow in
      drop  is required  per unit length  of  conduit, if  the annulus  a  thin slit  of  thickness IB the friction  factor  is / = 12/Re, if
      is horizontal? Use Eq. 6A.7-2.                   the  Reynolds  number is  defined  as  Re = 2B(v )p//A.  Com-
                                                                                            z
      (c)  Repeat  (b) using  the  "mean hydraulic  radius"  empiri-  pare  this  result  for  / with  what  one  would  get  from  the
      cism.                                            mean hydraulic radius empiricism.
      6A.8  Force  on  a  water  tower  in  a  gale.  A  water  tower  6B.4  Friction factor  for  a rotating disk. 3  A  thin  circular
      has a spherical storage tank 40 ft in diameter. In a 100-mph  disk  of  radius  R is immersed  in a large  body  of  fluid  with
      gale what  is  the force  of  the wind  on the spherical  tank at  density p and viscosity  /x. If a torque T  is required to make
                                                                                     z
      0°C? Take the density  of  air to be  1.29  g/liter  or 0.08  lb/ft 3  the  disk  rotate at an angular  velocity  ft,  then a friction  fac-
      and  the viscosity  to be 0.017 cp.              tor/may  be defined  analogously  to Eq. 6.1-1 as  follows,
      Answer: 17,000  Ц                                                  T /R  = AKf            (6B.4-1)
                                                                           z
      6A.9  Flow  of  gas  through a packed column.  A horizon-  where  reasonable  definitions  for  К and A  are К  = ^p(£lR) 2
                                                                  2
      tal  tube with diameter 4 in. and length 5.5  ft is packed  with  and  A  =  2(TTR ).  An  appropriate  choice  for  the  Reynolds
                                                                                 2
      glass spheres  of  diameter  1/16  in., and the void  fraction  is  number  for  the system  is Re =  R ftp//x.
      0.41.  Carbon dioxide  is  to be pumped  through the tube at  For  laminar  flow,  an  exact  boundary  layer  develop-
      300K,  at  which  temperature  its  viscosity  is  known  to  be  ment  gives
      1.495  X  10~ 4  g/cm  •  s.  What  will  be  the  mass  flow  rate  T z  =  0.6167rpR V/xft7p  (6B.4-2)
                                                                                 4
      through  the  column  when  the  inlet  and  outlet  pressures
      are 25 atm and 3 atm,  respectively?
      Answer: 480  g/s                                    2  H. Schlichting, Boundary-Layer Theory, McGraw-Hill, New
                                                       York, 7th edition  (1979), Chapter  XXI.
                                                          3
                                                            T. von Karman, Zeits. fur angew. Math. u. Mech., 1, 233-252
           D. M. Meter and R. B. Bird, AIChE  Journal, 7, 41-45 (1961).  (1921).
         1
   205   206   207   208   209   210   211   212   213   214   215