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As we have seen, a two-dimensional velocity field in which the flow is everywhere parallel to the
-
plane, and there is
no variation along the
-direction, takes the form
 |
(5.16) |
Moreover, if the flow is irrotational then
is automatically satisfied by writing
, where
is termed the velocity potential. (See Section 4.15.) Hence,
On the other hand, if the flow is incompressible then
is automatically
satisfied by writing
, where
is termed the
stream function. (See Section 5.2.) Hence,
Finally, if the flow is both irrotational and incompressible then Equations (5.17)-(5.18) and
(5.19)-(5.20) hold simultaneously, which implies that
It immediately follows, from the previous two expressions, that
 |
(5.23) |
or
 |
(5.24) |
Likewise, it can also be shown that
 |
(5.25) |
We conclude that, for two-dimensional, irrotational, incompressible flow, the velocity potential and the stream function
both satisfy Laplace's equation.
Equations (5.21) and (5.22) also imply that
 |
(5.26) |
In other words, the contours of the velocity potential and the stream function cross at right-angles.
Next: Two-Dimensional Uniform Flow
Up: Two-Dimensional Incompressible Inviscid Flow
Previous: Two-Dimensional Flow
Richard Fitzpatrick
2016-03-31