Page 46 - Mechanical Engineers Reference Book
P. 46

Principles of  thermodynamics  1/35

     which  intercept  the  stream  lines  at  right  angles  to  form  an   the  extensive  use  of  ‘coefficients’ (discharge  especially)  to
     orthogcinal  network  of  characteristic  pattern  for  each  flow   account  for  effects  which  are  difficult  to  model  matnema-
     field.                                         tically.  However,  almost  ail  fluid  mechanics  equations  in
       From equations  (1.124) and (1.127) it can be seen that   common  use  are  based  on  the  conservation  of  energy.  the
                                                    conservation of  momentum or the fact that the rate of  change
                                           (1.130)   of  momentum  may be equated to an applied force, usually a
                                                    pressure  force.  The  experimental  checking  and  empirical
                                                    amendment  to  derived  formulae  is  just  good  engineering
     which are the Cauchy-Rieman  equations. In such flow fieids   practice.
     the Laplace equations for d and $ must both be satisfied:   This  section  does  not  provide  rigorous  derivations  of  the
     v2+ = 13; and v*$ = o                 (1.131)   various equations quoted. Some appreciation of  such deriva-
                                                    tions may be required in order to establish the limitations and
     Because the fluid is ideal, the Bernoulli equation (1.37) may   modifications  necessary for the  application  of  the  equations,
     be readily applied between points in the field, both along and   especially to non-standard  situations. For this. standard  text-
     across the stream lines.                       books on fluid mechanics as listed below should be consulted.

     1.5.9.3  Flow patterns                         Further reading
     Examples  of  simple  flow patterns are  shown  in  Figure  1.48   General fluid mechanics
     with  the  equations  to  their  stream  functions  and  velocity   Douglas. J. F.. Gasiorek, J. M. and Swaffield, J. A,. Mechanics of
     potentials.  A source is mathematically  a point  at which fluid   Fluids, third edition, Pitman, London (1986)
     appears  and  flows  radially  outwards.  A  sink is  a  negative   Walshaw, A. C. and Jobson, D. A,, Mechanics of Fluids. third
     source  at which fluid flows radiaily inwards to disappear  at a   edition, Longman, London (1979)
     point  (similar  to the  plug  hole  in  a  domestic  sink,  where,   Ireland, J. W., Mechanics of  Fluids, Butterworths, London (1971)
     however,  there  is  a  vortex  superposed  to  produce  a  spiral   Reference tables
                                                    Houghton, E. L. and Brock. A. E., Tables for the Compressible
     vortex or whirlpool). A vortex is flow in concentric circles with   Flow of Dry Air, Edward Arnold, London (1961)
     no radial flow. A doublet is the superposilion of a source and a   Rogers, G. F. C. and Mayhew, Y. R., Thermodynamic and
     sink of  equal strength rn, initially a distance 20 apart brought   Transport Properties  of  Fluids, third edition, Blackwell, Oxford
     infinitely close together  so that the product  of  their  strength   (1980)
     and the  distance between them remains a constant k. k is the   Additional computer solutions
     strength of  the donblet and is equal to 2am.   Smith, P. D., BASIC Hydraulics, Butterworths, London (1982)
       This is a mathematical concept which is apparently imprac-   Boundary layer flow
     tical  but  yields  a  useful  flow  pattern.  It  is  often  used  in   Schlicting, H., Boundary Layer  Theory, fourth edition,
     combination  with other simple patterns.        McGraw-Hill, New  York (1960)
                                                    Ideal fluid flow
                                                    O‘Neill, M. E. and Chorlton, E’.,  Ideal and Incompressible Fluid
     1.5.9.4  Modelling                              Dynamics, Ellis Horwood, Chichester (1986)
                                                    For students preparing for examinations
     Since there can be no flow across a stream line and the fluid is   Douglas. J. F., Solutions of  Problems in Fluid Mechanics, Parts 1
     assume’d inviscid,  any  stream  line  in  a  flow pattern  may  be   and 2, third edition, Pitman, London (1987)
     replaced  by  a solid  surface with  no  effect on the rest  of  the   Brasch, D. J. and Whyman, D., Problems in Fluid Flow, Edward
     pattern.  A  stream  line  forming  a  closed  contour  may  be   Arnold, London (1986)
     replaced by a solid body to model the flow pattern around  a
     body  of  the  same  shape. This provides  a  method  of  writing
     mathematical  models  to  describe  the  flow  streams  around   1.6.  Principles of thermodynamics
     various shapes.
       The limitations of  the model must be understood, and the   1.6.1  Introduction
     effects of rotation and viscosity particularly  considered, when
     applying the analysis to real situations. For example, the flow   Thermodynamics  is  concerned  with  energy  transfers  in  pro-
     round a cylinder may be modelled by a combination of doublet   cesses. Two modes of  transfer are recognized: work (transfer)
     and  parallel  flow.  The  drag  and  lift  forces  calculated  by   and heat (transfer). From the mechanical engineer’s viewpoint
     integrating the resulting pressure forces at the cylinder surface   the  main  interest  is the  production  of  shaft  power  (rate  of
     appear to be zero. This is obviously not correct.   work transfer) by a machine to which the energy is supplied by
       In the  real  situation  the  viscosity of  the  fluid  produces  a   heat  transfer  obtained  directly or indirectly from the combu-
     boundary  layer  at  the  cylinder  surface.  which,  because  of   stion  of  a  hydrocarbon  fuel  in  air.  Before  proceeding.  the
     curvature, separates from the  surface  to  form  a  wake.  The   terminology used in thermodynamics must be defined.
     presence  of  the  wake  disturbs  the  downstream  flow pattern   The particular part of  the working substance under conside-
     2nd  the  form  drag  force  is  a  consequence.  Viscosity  also   ration  is  called  the  system,  and  this  is  separated  from  the
     introduces  a surface friction drag.           surroundings by a boundary. In the closed or non-flow system
       The shedding of  vortices from the cylinder surface into the   the mass of working substance is constant, but in the open or
     wake also produces alternate positive and negative lift forces,   flow system  there  is  a  mass  flow  rate  across  the  boundary.
     which are not predicted  by the ideal flow analysis,  although   Some processes  in reciprocating plant  may be considered by
     telegraph wires may often be observed vibrating in the wind.   non-flow  analysis but  in  steam plant, for example,  most  are
                                                    considered by flow analysis. The state of  a system is defined by
                                                    the  properties  (pressure,  temperature,  etc.).  Properties  are
     1.5.18 Conclusion
                                                    normally  expressed specifically  (Le. per unit  mass) to enable
     Fluid  mechanics  is  often  regarded  as  an  empirical  subject   charts or tables to be used. The state of  simple substances can
     which makes use of  formulae based only on observed exper-   be described by two independent properties, but complex ones
     imental results. This misconception is further compounded by   such  as mixtures  need  more definition.  A change of  state  is
   41   42   43   44   45   46   47   48   49   50   51