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§11.4  Use of the Equations of Change to Solve  Steady-State Problems  349

                               To  determine that function,  we  have  to make  experimental  measurements  or solve Eqs.
                                                  3
                            11.4-44  to 4. In 1881, Lorenz  obtained  an approximate solution  to these equations and  found
                            С  = 0.548. Later, more refined  calculations  gave the following  dependence of С on Pr:
                                                             4
                                          Pr  0.73 (air)  1    10    100   1000   00
                                          С     0.518  0.535  0.620  0.653  0.665  0.670

                           These values  of  С are nearly  in exact agreement with  the best  experimental  measurements in
                                                             9
                           the  laminar flow range  (i.e., for  GrPr <  10 ). 5
       EXAMPLE   11.4-6     Develop equations  for  the relationship  of  local pressure  to density  or temperature in a stream
                            of ideal gas  in which the momentum flux  т and the heat flux  q are  negligible.
      Adiabatic  Frictionless
      Processes in  an      SOLUTION
      Ideal  Gas
                           With  т and q neglected, the equation  of energy  [Eq. (/) in Table  11.4-1] may be rewritten as
                                                           DT
                                                              -
                                                       nC  —  _{d  In  V\  D P                 (11.4-52)
                                                                 d\x\  T) Dt
                                                                       p
                            For  an  ideal  gas,  pV  = RT/M,  where  M  is  the molecular  weight  of  the gas,  and  Eq.  11.4-52
                           becomes
                                                                                               (11.4-53)
                                                               Dt   Dt
                            Dividing  this equation by  p and  assuming  the molar heat capacity  C p  = MC p  to be constant,
                            we  can again use the ideal gas  law  to get

                                                                                               (11.4-54)

                            Hence the quantity  in parentheses  is a constant along  the path  of a fluid  element, as  is  its an-
                            tilogarithm, so that we  have
                                                          C,,/R -i  instant                    (11.4-55)
                                                         T    p   =
                            This  relation  applies  to  all  thermodynamic states  p, T that  a  fluid  element  encounters  as  it
                            moves  along with the  fluid.
                               Introducing  the definition  у  = C /C v  and  the ideal  gas  relations  C p  -  C v  = R and  p  =
                                                          p
                           pRT/M, one obtains the related  expressions
                                                                                               (11.4-56)
                            and
                                                            pp  y  = constant                  (11.4-57)
                            These last  three equations  find  frequent  use  in the study  of  frictionless  adiabatic processes  in
                            ideal gas  dynamics. Equation 11.4-57 is a famous  relation well worth remembering.


                               3
                                L. Lorenz,  Wiedemann's  Ann.  der Physik  u. Chemie, 13,422-^147,  582-606 (1881). See also  U. Grigull,
                            Die Grundgesetze der  Warmeiibertragung, Springer-Verlag,  Berlin, 3rd edition  (1955), pp.  263-269.
                               4  See  S. Whitaker,  Fundamental  Principles of Heat Transfer, Krieger, Malabar  Fla. (1977), §5.11. The
                            limiting  case  of  Pr  —» °°  has been worked  out numerically by  E. J. LeFevre [Heat Div. Paper 113, Dept.
                            Sci. and Ind. Res., Mech. Engr. Lab. (Great Britain), Aug.  1956] and  it was  found  that
                                                           0.5028          1.16
                                                    дУ)               r,=0  /1/4
                            Equation  11.4-51 a corresponds  to the value  С = 0.670 above.  This result has been  verified  experimentally
                            by  C. R. Wilke, C. W. Tobias, and  M. Eisenberg,  /. Electrochem. Soc,  100, 513-523  (1953), for  the  analogous
                            mass  transfer  problem.
                               5
                                For an analysis  of  free  convection  in three-dimensional creeping flow, see W.  E. Stewart, Int. ]. Heat
                            and Mass  Transfer, 14,1013-1031  (1971).
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