Page 126 - Bird R.B. Transport phenomena
P. 126

Problems  111

      the  equations  of  change: (i) we  assume  that the speed  v  is  (e)  Integrate [(p + r )  -  p ]  over  the moving-disk  surface
                                                  0                   zz   atm
      so  slow  that all  terms  containing time  derivatives  can  be  to  find  the total force needed to maintain the disk motion:
      omitted; this  is  the so-called  "quasi-steady-state"  assump-
      tion; (ii) we use the fact that H  «  R to neglect quite a  few        ЗТТ/JLVQR 4
                             o                                          F(t)  =               (3C.1-14)
      terms  in  the  equations  of  change  by  order-of-magnitude           2[H(0]  3
      arguments. Note that the rate  of  decrease  of  the fluid  vol-  This  result  can  be  used  to  obtain  the  viscosity  from  the
                              2
      ume  between  the disks  is  7rR v , and  that this  must  equal
                               0                       force and velocity measurements.
      the  rate  of  outflow  from  between  the  disks,  which  is
      2irRH(v r )\ r=R .  Hence                        (f)  Repeat the analysis  for  a viscometer  that is operated in
                                                       such  a  way  that  a  centered, circular  glob  of  liquid  never
                                                       completely  fills  the space  between  the two  plates.  Let the
                                              (3C.1-1)
                               2ВД)                    volume  of the sample be V and obtain
      We  now  argue  that v (r,  z) will  be  of  the order  of  magni-
                       r                                                                      (3C.1-15)
      tude  of (v )\ =R and that v {r, z) is  of the order  of magnitude     2тг[Я(0] 5
               r
                          z
             r
      of v , so that
         0
                                                       (g)  Repeat  the  analysis  for  a  viscometer  that  is  operated
                   v  «  (R/H)v )  v  «  -i  (3C.1-2,3)  with  constant applied  force, F .  The viscosity  is  then to be
                    r        0   z                                             o
                                                       determined by  measuring Я  as  a function  of  time, and the
      and  hence  \v \ «  v,..  We  may  now  estimate  the order  of  upper-plate velocity  is not a constant. Show that
                z
      magnitude  of  various  derivatives  as  follows:  as  r  goes
      from 0 to R, the radial velocity  v  goes from zero to approx-    1     1  ,  4F f
                                                                                    0
                               r                                                              (3C.1-16)
      imately (R/H)v .  By this kind  of reasoning we  get            [H(t)] 2
                  0
                  dv r  ^  (R/H)v 0  -  0 _  v 0  (ЗСЛ-4)  3C.2  Normal  stresses  at  solid  surfaces  for  compress-
                                                       ible fluids.
                                                                 Extend example
                                                                                   to compressible
                                                                               3.1-1
                                                                                                 fluids.
                  ~dr~    R^O     = H
                                                       Show that
                  dv z  (-v )  -  0  v 0                          т |  = (!/*  +  *)(<? In  p/dt)\  (3C.2-1)
                         0
                   dz   H  -  0    H'         (ЗСЛ-5)              22 г=0                z=0
                                                       Discuss the physical  significance  of this result.
      (a)  By  the  above-outlined  order-of-magnitude  analysis,
      show  that the continuity equation and the r-component of  3C.3  Deformation  of  a fluid line  (Fig.  3C.3).  A  fluid  is
      the  equation of motion become (with g  neglected)  contained  in  the annular  space  between  two  cylinders  of
                                    z
                                                       radii KR and R. The inner cylinder  is made to rotate with a
      continuity:                             (3C.1-6)  constant  angular  velocity  of  ft,.  Consider  a  line  of  fluid
                                                       particles in the plane z  = 0 extending from  the inner cylin-
                                                       der  to the outer cylinder and initially  located at в  = 0, nor-
      motion                                  (3C.1-7)
                           dr    dz L                  mal  to the two  surfaces.  How  does  this  fluid  line  deform
                                                       into a curve  0(r, f)? What  is the length,  /, of  the curve  after
      with the boundary conditions                     N  revolutions  of the inner cylinder? Use Eq. 3.6-32.
      B.C.I:  atz  = 0,    v r  = 0,  v  = 0  (3C.1-8)
                                    z                  Ansiver:±=  '  M  '  1 б 7 г 2 Д Р
      B.C. 2:  at z =  Ш ) ,  v  = 0,  v  =  -v  (3C.1-9)
                           r        z    0
      B.C.3:  at  r =  R,  p  =  p a t m     (3C.1-10)
      (b)  From Eqs. 3C.1-7 to 9 obtain
                         1  /^p\                                                  Fluid curve
                     iV = 7г-  К -  zfe  -  Я)  (ЗС.1-11)                          atf  >0
                        2/г  \dr/
      (c)  Integrate Eq. 3C.1-6 with respect to z and substitute the
      result from  Eq. З.СЛ-11 to get
                          Я  3  1  d  (  dp\                                          Fluid line
                     0    12/x  r  dr \  dr)                                           atf  = 0
                                                                                    Inner cylinder
      (d)  Solve Eq. 3C.1-12 to get the pressure  distribution  Fixed outer      rotating with angular
                                                             cylinder                velocity Qj
                          3/xi;R :
                             0
                 V  =  Patm  ^[-(5)']        (3C.1-13)  Fig.  3C.3.  Deformation of a fluid  line in Couette flow.
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