Paper 1, Section II, C

Fluid Dynamics
Part IB, 2019

Explain why the irrotational flow of an incompressible fluid can be expressed in terms of a velocity potential ϕ\phi that satisfies Laplace's equation.

The axis of a stationary cylinder of radius aa coincides with the zz-axis of a Cartesian coordinate system (x,y,z)(x, y, z) with unit vectors (ex,ey,ez)\left(\mathbf{e}_{x}, \mathbf{e}_{y}, \mathbf{e}_{z}\right). A fluid of density ρ\rho flows steadily past the cylinder such that the velocity field u\mathbf{u} is independent of zz and has no component in the zz-direction. The flow is irrotational but there is a constant non-zero circulation

udr=κ\oint \mathbf{u} \cdot d \mathbf{r}=\kappa

around every closed curve that encloses the cylinder once in a positive sense. Far from the cylinder, the velocity field tends towards the uniform flow u=Uex\mathbf{u}=U \mathbf{e}_{x}, where UU is a constant.

State the boundary conditions on the velocity potential, in terms of polar coordinates (r,θ)(r, \theta) in the (x,y)(x, y)-plane. Explain why the velocity potential is not required to be a single-valued function of position. Hence obtain the appropriate solution ϕ(r,θ)\phi(r, \theta), in terms of a,Ua, U and κ\kappa.

Neglecting gravity, show that the net force on the cylinder, per unit length in the zz-direction, is

ρκUey-\rho \kappa U \mathbf{e}_{y}

Determine the number and location of stagnation points in the flow as a function of the dimensionless parameter

λ=κ4πUa\lambda=\frac{\kappa}{4 \pi U a}