6. Consider a potential vortex of strength m, located at a distance h above a stationary wall. Determine the complex potential function and derive the velocity and pressure fields. Is the vortex stationary?
Let's assume the origin at center of the wall and the vortex at .
Let the velocity and pressure far from the vortex is and .
The potential of uniform flow will be
Since, the rotation of the vortex is not given, so we will account for both rotation -
for counterclockwise rotation of flow,the potential function is
for clockwise rotation, the potential function will be-
where, and in cartesian coordinate is given as -
Thus the complex potential function for the vortex will be -
The x component of the velocity field is given as -
The y component of the velocity will be zero as no flow throgh the wall can occur.
The pressure field across the wall can be calculated using Bernoulli's equation -
The difference in pressure results a net force along y direction to the vortex, which will keep oscillating the vortex, depending on its distance from wall.
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