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u , = 1 r ψ θ , u θ = - ψ r

The reader may find useful the general rule for two-dimensional flow, that differentiation of ψ in a certain direction gives the velocity component 90 degree in the clockwise sense from that direction.

Finally, for this case of two-dimensional flow of incompressible fluid, we should note the possibility that ψ is a many-valued function of position. For suppose that across some closed inner geometrical boundary there is a net volume flux m ; this flux might be due to an effective creation of fluid within the inner boundary (as when a tube discharges fluid into this region) or to change of volume of the part of the enclosed region not occupied by the fluid (as when a gaseous cavity surrounded by water expands or contracts).

If now we choose two different paths joining the two points 0 and P which together make up a closed curve enclosing the inner boundary, the fluxes of volume across the two joining curves differ by an amount m (or, more generally, by p m , where p is the number of times the combined closed curve passes round the inner boundary). The value of ψ - ψ o at the point P thus depends on the choice of path joining it to the reference point 0, and may take any one of a number of values differing by multiples of m . This kind of many-valuedness of a scalar function related to the velocity distribution in a region which is not singly-connected will be described more fully in § 2.8. It is not confined to two-dimensional flow, although that is the context in which it occurs most often.

If now the flow has symmetry about an axis, the mass-conservation equation for an incompressible fluid takes the form

· u = u x + 1 σ ( σ v ) σ = 0

in terms of cylindrical co-ordinates ( x , σ , φ ) with corresponding velocity components ( u , v , w ) , the axis of symmetry being the line σ = 0 . This relation ensures that σ u δ σ - σ v δ x is an exact differential, equal to δ ψ say. Then

u = 1 σ ψ σ , v = - 1 σ ψ x

and the function ψ ( x , σ , t ) is defined by

ψ - ψ o = σ ( u d σ - v d x ) ,

where the line integral is taken along an arbitrary curve in an axial plane joining some reference point 0 to the point P with co-ordinates ( x , σ ) . It will be noticed that the azimuthal component of velocity w does not enter into the mass-conservation equation in a flow field with axial symmetry and cannot be obtained from ψ .

Again it is possible to interpret ψ both as a measure of volume flux and as one component of a vector potential. The flux of fluid volume across the surface formed by rotating an arbitrary curve joining 0 to P in an axial plane, about the axis of symmetry, the flux again being reckoned as positive when it is in the anti-clockwise sense about P , is 2 π -times the right-hand side of (2.2.12). Lines in an axial plane on which ψ is constant are everywhere parallel to the vector ( u , v , o ), and can be described as `streamlines of the flow in an axial plane'. ψ is here termed the Stokes stream function . A sketch of lines on which ψ is constant, with the same increment in ψ between all pairs of neighboring lines (see figure 2.5.2 for an example), does not give quite as direct an impression of the distribution of velocity magnitude here as in two-dimensional flow, owing to the occurrence of the factor 1 / σ in the expressions for u and v in (2.2.11). The relations (2.2. 11) are readily seen to be equivalent to

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Source:  OpenStax, Transport phenomena. OpenStax CNX. May 24, 2010 Download for free at http://cnx.org/content/col11205/1.1
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