Page 30 - Bird R.B. Transport phenomena
P. 30

§1.1  Newton's Law of Viscosity (Molecular Transport of Momentum)  15

                           Table  1.1-4  Viscosities of Some Liquid Metals

                                    Temperature    Viscosity
                           Metal       T(°C)      /x (mPa  • s)

                           Li          183.4        0.5918
                                       216.0        0.5406
                                       285.5        0.4548
                           Na          103.7        0.686
                                       250          0.381
                                       700          0.182
                           К            69.6        0.515
                                       250          0.258
                                       700          0.136
                           Hg          -20          1.85
                                        20          1.55
                                       100          1.21
                                       200          1.01
                           Pb          441          2.116
                                       551          1.700
                                       844          1.185
                           Data taken from  The Reactor Handbook, Vol.  2, Atomic
                           Energy Commission AECD-3646, U.S. Government
                           Printing Office,  Washington,  D.C. (May 1955), pp. 258
                           et seq.


                           given  for  pure fluids  at 1 atm pressure.  Note that for  gases at low  density,  the viscosity
                            increases  with  increasing  temperature, whereas  for  liquids  the viscosity usually decreases
                           with  increasing  temperature. In gases the momentum is transported by  the molecules in
                           free  flight  between  collisions, but  in liquids  the transport takes  place predominantly  by
                           virtue  of  the intermolecular  forces  that pairs  of  molecules  experience  as they wind  their
                           way  around  among  their  neighbors.  In §§1.4  and  1.5  we  give  some  elementary  kinetic
                            theory arguments  to explain  the temperature dependence of viscosity.

                                                                      2
       EXAMPLE 1.1-1       Compute the steady-state momentum flux т  in lty/ft  when the lower plate velocity V in Fig.
                                                               ух
                            1.1-1 is 1 ft/s in the positive x direction, the plate separation У is 0.001 ft, and the fluid viscos-
      Calculation of       ity  ix is 0.7 cp.
      Momentum Flux
                            SOLUTION
                           Since т  is desired  in British units, we should  convert the viscosity into that system of units.
                                 ух
                                                                                  5
                           Thus, making use of Appendix  F, we find  /x = (0.7 cp)(2.0886 X 10" ) = 1.46 X 10~  lb, s/ft .
                                                                                                     2
                                                                                               5
                           The  velocity profile is linear so that
                                                   dv   bv   -1.0 ft/s
                                                     x  =  x  =      =  -lOOOs" 1                (1.1-5)
                                                   dy   Ду  ~  0.001 ft
                           Substitution into Eq.  1.1-2 gives
                                                                                   2
                                                                5
                                         r  = -fi^  = -(1.46 X 10~ )(-1000) = 1.46 X 10" lb/ft 2  (1.1-6)
                                          yx
                                                 ay                                 '
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