Paper 3, Section II, A

Fluid Dynamics II | Part II, 2019

For a fluid with kinematic viscosity ν\nu, the steady axisymmetric boundary-layer equations for flow primarily in the zz-direction are

uwr+wwz=νrr(rwr)1r(ru)r+wz=0\begin{aligned} u \frac{\partial w}{\partial r}+w \frac{\partial w}{\partial z} &=\frac{\nu}{r} \frac{\partial}{\partial r}\left(r \frac{\partial w}{\partial r}\right) \\ \frac{1}{r} \frac{\partial(r u)}{\partial r}+\frac{\partial w}{\partial z} &=0 \end{aligned}

where uu is the fluid velocity in the rr-direction and ww is the fluid velocity in the zz-direction. A thin, steady, axisymmetric jet emerges from a point at the origin and flows along the zz-axis in a fluid which is at rest far from the zz-axis.

(a) Show that the momentum flux

M:=0rw2drM:=\int_{0}^{\infty} r w^{2} d r

is independent of the position zz along the jet. Deduce that the thickness δ(z)\delta(z) of the jet increases linearly with zz. Determine the scaling dependence on zz of the centre-line velocity W(z)W(z). Hence show that the jet entrains fluid.

(b) A similarity solution for the streamfunction,

ψ(x,y,z)=νzg(η) with η:=r/z\psi(x, y, z)=\nu z g(\eta) \quad \text { with } \quad \eta:=r / z

exists if gg satisfies the second order differential equation

ηgg+gg=0\eta g^{\prime \prime}-g^{\prime}+g g^{\prime}=0

Using appropriate boundary and normalisation conditions (which you should state clearly) to solve this equation, show that

g(η)=12Mη232ν2+3Mη2g(\eta)=\frac{12 M \eta^{2}}{32 \nu^{2}+3 M \eta^{2}}

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