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Complex Velocity
Equations (5.17), (5.20), and (6.15) imply that
 |
(6.35) |
Consequently,
is termed the complex velocity. It follows that
 |
(6.36) |
where
is the flow speed.
A stagnation point is defined as a point in a flow pattern at which the flow speed,
, falls to zero. (See Section 5.8.)
According to the previous expression,
 |
(6.37) |
at a stagnation point. For instance, the stagnation points of the flow pattern produced when a cylindrical obstacle of radius
, centered on the origin, is placed in a uniform flow of speed
, directed parallel to the
-axis, and the circulation of the flow around is cylinder is
, are found by setting the derivative of the complex potential (6.32) to zero.
It follows that the stagnation points satisfy the quadratic equation
 |
(6.38) |
The solutions are
 |
(6.39) |
where
,
with the proviso that
, because the region
is occupied by the cylinder. Thus, if
then there are two stagnation points on the surface of the cylinder at
and
.
On the other hand, if
then there is a single stagnation point below the cylinder at
and
.
According to Section 4.15, Bernoulli's theorem in an steady, irrotational, incompressible fluid takes the form
 |
(6.40) |
where
is a uniform constant. Here, gravity (and any other body force) has been neglected. Thus, the
pressure distribution in such a fluid can be written
 |
(6.41) |
Next: Method of Images
Up: Two-Dimensional Potential Flow
Previous: Complex Velocity Potential
Richard Fitzpatrick
2016-03-31