Consider an incompressible viscous fluid of kinematic viscosity $ν$ , dynamic viscosity $µ$ and density $ρ$ . A viscous boundary layer is located over a solid surface at $y = 0$ and $x > 0$. The flow in the boundary layer must match with the constant inviscid bulk velocity $U$. The steady two-dimensional boundary-layer equations are $$\frac{∂ u}{ ∂ x} + \frac{∂ v}{ ∂ y} = 0$$ $$ρ \bigg( u \frac{∂ u }{∂ x} +v \frac{∂ u }{∂ y} \bigg)= µ \frac{∂ ^2u }{∂ y^2}$$ where $u(x,y)$ is the horizontal velocity and $v(x,y)$ the vertical velocity.
(i) State the boundary conditions on $u$ and $v$ along $y = 0$ and $x > 0$.
(ii) State the far-field condition on $u$ as $y→∞$.
It says "The flow in the boundary layer must match with the constant inviscid bulk velocity $U$" so does this mean that the resultant of the $u$ and $v$ velocity components should be equal to $U$?
Then for (i) $u(x,y=0)=v(x,y=0)=U/\sqrt2$?
For (ii), is the far field condition just $u \rightarrow 0$ as $y \rightarrow \infty$?
