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§4.3 Flow of Inviscid Fluids by Use of the Velocity Potential 127<br />

We want to solve Eqs. 4.3-3 to 5 to obtain v x<br />

, v y<br />

, and 2P as functions of x and y. We<br />

have already seen in the previous section that the equation of continuity in two-dimensional<br />

flows can be satisfied by writing the components of the velocity in terms of a<br />

stream function ф{х, у). However, any vector that has a zero curl can also be written as the<br />

gradient of a scalar function (that is, [V X v] = 0 implies that v = —Уф). It is very convenient,<br />

then, to introduce a velocity potential ф(х, у). Instead of working with the velocity<br />

components v x<br />

and v y<br />

, we choose to work with ф(х, у) and ф{х, у). We then have the following<br />

relations:<br />

дф дф<br />

(stream function) v x<br />

= —r- v u<br />

= — (4.3-6,7)<br />

dy<br />

(velocity potential) v x<br />

= ~ v y<br />

= ~ (4.3-8,9)<br />

Now Eqs. 4.3-3 and 4.3-4 will automatically be satisfied. By equating the expressions for<br />

the velocity components we get<br />

дф дф дф дф<br />

-г- = -т- and — = -— (4.3-10,11)<br />

дХ ду ду дХ<br />

These are the Cauchy-Riemann equations, which are the relations that must be satisfied by<br />

the real and imaginary parts of any analytic function 3 w{z) = ф(х, у) + iiftix, у), where z =<br />

x + iy. The quantity w(z) is called the complex potential. Differentiation of Eq. 4.3-10 with<br />

respect to x and Eq. 4.3-11 with respect to у and then adding gives V 2 = 0. Differentiating<br />

with respect to the variables in reverse order and then substracting gives Vfy = 0.<br />

That is, both ф(х, у) and ф{х, у) satisfy the two-dimensional Laplace equation. 4<br />

As a consequence of the preceding development, it appears that any analytic function<br />

zv(z) yields a pair of functions ф{х, у) and ф{х, у) that are the velocity potential and<br />

stream function for some flow problem. Furthermore, the curves ф(х, у) = constant and<br />

ф{х, у) = constant are then the equipotential lines and streamlines for the problem. The velocity<br />

components are then obtained from Eqs. 4.3-6 and 7 or Eqs. 4.3-8 and 9 or from<br />

^T=-v x<br />

+ iv 4<br />

(4.3-12)<br />

J<br />

az '<br />

in which dw/dz is called the complex velocity. Once the velocity components are known,<br />

the modified pressure can then be found from Eq. 4.3-5.<br />

Alternatively, the equipotential lines and streamlines can be obtained from the inverse<br />

function z(w) = х{ф, ф) + гу(ф, ф), in which z(w) is any analytic function of w. Between<br />

the functions х{ф, ф) and у{ф, ф) we can eliminate ф and get<br />

J<br />

dX<br />

F(x,y,

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