Flow Past a Source

Satisfaction

When a uniform flow is added to that due to a source -
  • fluid emitted from the source is swept away in the downstream direction
  • stream function and velocity potential for this flow will be the sum of those for uniform flow and source
Stream function;     
Velocity Potential;  
So                           
and                          
Fig 23.1  The streamlines of the flow past a line source for equal increments of 2πψ/q
The Plane coordinates are x/a, y/a where a=k/u
Explanation of Figure
  • At the point x = -a, y = 0 fluid velocity is zero.
  • This is called stagnation point of the flow
  • Here the source flow is turned around by the oncoming uniform flow
  • The parabolic streamline passing through stagnation point  seperates uniform flow from the source flow.
  • The streamline becomes parallel to x axis as 
Flow Past Vortex
when uniform flow is superimposed with a vortex flow -
  • Flow will be asymmetrical about x - axis
  • Again stream function and velocity potential will be the sum of those for uniform flow and vortex flow
Stream Function:   
Velocity Potential:   
so that;