Page 105 - Aerodynamics for Engineering Students
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88  Aerodynamics for Engineering Students














                                            ' Bundle of vortex tubes
                Fig. 2.27




                  Circulation can be regarded  as a measure  of the combined  strength  of  the total
                number of vortex lines passing through A. It is a measure of the vorticityjlux carried
                through A by these vortex lines. The relationship between circulation and vorticity is
                broadly  similar to  that  between momentum  and velocity or that between internal
                energy and temperature. Thus circulation is the property of the region A bounded by
                control  surface  C, whereas vorticity  is a  flow variable,  like velocity, defined  at  a
               point.  Strictly  it  makes  no  more  sense  to  speak  of  conservation,  generation,  or
                transport of vorticity than its does to speak of conservation, generation, or transport
                of velocity. Logically these terms should be applied to circulation just as they are to
               momentum rather than velocity. But human affairs frequently defy logic and aero-
               dynamics is no exception. We have become used to speaking in terms of conservation
               etc.  of  vorticity.  It  would  be  considered  pedantic  to  insist  on  circulation  in  this
               context,  even  though  this  would  be  strictly  correct.  Our  only  motivation  for
               making  such fine distinctions here is to  elucidate the meaning and significance of
               circulation. Henceforth  we  will adhere to the common usage of  the terms vorticity
                and circulation.
                  In two-dimensional  flow, in the absence of the effects of viscosity, circulation is
               conserved. This can be expressed mathematically as follows:


                                                                                  (2.82)

               In view  of what was written in  Section 2.7.6 about the link  between vorticity  and
               viscous effects, it may seem somewhat illogical to neglect such effects in Eqn (2.82).
               Nevertheless, it is often a useful approximation to use Eqn (2.82).
                 Circulation  can  also  be  evaluated  by  means  of  an  integration  around  the
               perimeter  C. This  can  be  shown  elegantly  by  applying  Stokes  theorem  to  Eqn
               (2.8 1); thus


                                                                                  (2.83)

               This commonly serves as the definition of circulation in most aerodynamics text.
                 The concept of circulation is central to the theory of lift. This will become clear in
                Chapters 5 and 6.
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