A microfluidic chip carries an aqueous buffer of dynamic viscosity and density along…

PHYSICS · Multi-part · Fermi University Physics · Mathematical Methods for Physics · Fluids & Continuum Physics · Viscous flow and dynamical similarity

Fluids and Continuum Physics, Ch The Navier-Stokes equations and exact viscous solutions

Problem

A microfluidic chip carries an aqueous buffer of dynamic viscosity μ=1.2×10−3 Pa s\mu = 1.2\times10^{-3}\ \mathrm{Pa\,s} and density ρ=1000 kg m−3\rho = 1000\ \mathrm{kg\,m^{-3}} along a straight horizontal channel of circular cross-section, radius a=60 μma = 60\ \mu\mathrm{m} and length L=25 mmL = 25\ \mathrm{mm}. The flow is steady, smooth, layered, incompressible, unidirectional and fully developed, with no slip at the wall, so u(r)=(G/4μ)(a2−r2)u(r) = (G/4\mu)(a^{2}-r^{2}) with GG the uniform axial pressure gradient. The required volume flow rate is Q=2.0×10−9 m3 s−1Q = 2.0\times10^{-9}\ \mathrm{m^{3}\,s^{-1}}. In the plane containing the axis take xx along the flow and yy across it measured from the axis, so that there ux=(G/4μ)(a2−y2)u_x = (G/4\mu)(a^{2}-y^{2}) and uy=0u_y = 0. ((a)) Find the pressure difference needed between the ends of the channel. ((b)) At y=a/2y = a/2, find the rate-of-strain component exy=12(∂ux/∂y+∂uy/∂x)e_{xy} = \tfrac12(\partial u_x/\partial y + \partial u_y/\partial x) and the viscous shear stress τxy\tau_{xy}, giving magnitudes. ((c)) The vorticity ω=∇×u\boldsymbol{\omega} = \nabla\times\mathbf{u} of this planar flow varies linearly with yy. Using Chapter 8's result that the circulation round a flat loop equals the flux of vorticity through it, Γ=∫Aωz dA\Gamma = \int_A\omega_z\,\mathrm{d}A, find the magnitude of the circulation round a square loop of side d=4.0 μmd = 4.0\ \mu\mathrm{m} lying in this plane, with its centre at y=a/2y = a/2 and its sides parallel to the axes. In your working, state which terms of the Navier-Stokes equation vanish for this flow and why.

Browse the problem library