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The following boundary condition exists at the wall (y = 0) in a boundary layer:
1. u = U
2. \(\frac {dP}{dX}= -ve\)
3. τ0 = 0
4. u = 0, v = 0

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Correct Answer - Option 4 : u = 0, v = 0

Concept:

The point of separation may be defined as the limit between forward and reverse flow in the layers very close to the wall i.e. at the point at separation

\({\left( {\frac{{\partial u}}{{\partial y}}} \right)_{y = 0}} = 0\)

At boundary conditions and the equation ( simplifies since ∂u/∂t = 0.) Assuming Steady-state condition.

  • At the plate surface, there is no flow across it, which implies that v = 0 at y = 0. 
  • Due to the viscosity, we have the no-slip condition at the plate. In other words, u = 0 at y = 0. 
  • At infinity (outside the boundary layer), away from the plate, we have that u → U as y → infinity

 

For a given velocity profile, it can be determined whether the boundary has separated, or on the verge of separation, or will not separate from the following condition:

i) \({\left( {\frac{{\partial u}}{{\partial y}}} \right)_{y = 0}} < 0\) the flow has separated

ii) \({\left( {\frac{{\partial u}}{{\partial y}}} \right)_{y = 0}} = 0\) the flow is on the verge of separation.

ii) \({\left( {\frac{{\partial u}}{{\partial y}}} \right)_{y = 0}} > 0\) the flow will not separate or flow will remain attached with the surface.

 

<!--[if gte msEquation 12]>dPdX= -ve<![endif]--><!--[if !msEquation]--><!--[endif]-->

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