2.II.36B

Fluid Dynamics II
Part II, 2007

Viscous fluid is extracted through a small hole in the tip of the cone given by θ=α\theta=\alpha in spherical polar coordinates (R,θ,ϕ)(R, \theta, \phi). The total volume flux through the hole takes the constant value QQ. It is given that there is a steady solution of the Navier-Stokes equations for the fluid velocity u\mathbf{u}. For small enough RR, the velocity u\mathbf{u} is well approximated by u(A/R2,0,0)\mathbf{u} \sim\left(-A / R^{2}, 0,0\right), where A=Q/[2π(1cosα)]A=Q /[2 \pi(1-\cos \alpha)] except in thin boundary layers near θ=α\theta=\alpha.

(i) Verify that the volume flux through the hole is approximately QQ.

(ii) Construct a Reynolds number (depending on RR ) in terms of QQ and the kinematic viscosity ν\nu, and thus give an estimate of the value of RR below which solutions of this type will appear.

(iii) Assuming that there is a boundary layer near θ=α\theta=\alpha, write down the boundary layer equations in the usual form, using local Cartesian coordinates xx and yy parallel and perpendicular to the boundary. Show that the boundary layer thickness δ(x)\delta(x) is proportional to x32x^{\frac{3}{2}}, and show that the xx component of the velocity uxu_{x} may be written in the form

ux=Ax2F(η), where η=yδ(x)u_{x}=-\frac{A}{x^{2}} F^{\prime}(\eta), \quad \text { where } \quad \eta=\frac{y}{\delta(x)}

Derive the equation and boundary conditions satisfied by FF. Give an expression, in terms of FF, for the volume flux through the boundary layer, and use this to derive the RR dependence of the first correction to the flow outside the boundary layer.