Flow in stems and pipes II

If two sections of a fluid flow past one another with relative velocity, they will pull on one another with a drag force that is proportional to the fluid viscosity, η \eta , as well as to the change in velocity over the change in distance, i.e. the gradient v ( r ) \nabla v(r) .

Consider the diagram below, which crudely approximates fluid flowing down a pipe as three adjacent cylindrical layers flowing at velocities v ( r d r ) > v ( r ) > v ( r + d r ) v(r-dr)>v(r)>v(r+dr) . The flow of all three layers is out of the screen (as indicated by the white dot at the center).

Focusing on the middle layer, which travels with velocity v ( r ) v(r) , it feels a forward pull per unit area from the central layer (since v ( r d r ) > v ( r ) v(r-dr) > v(r) , given by η v ( r + d r ) v ( r ) d r \eta\frac{v(r+dr)-v(r)}{dr} .

In other words, the central layer is pulling the middle layer through some surface interaction, so that the total pull is given by η v ( r + d r ) v ( r ) d r S A \eta\frac{v(r+dr)-v(r)}{dr}S_A with S A S_A being the surface area of interaction between the two layers.

Similarly, the middle layer feels a backward pull from the top layer given by η v ( r d r ) v ( r ) d r S A \eta\frac{v(r-dr)-v(r)}{dr}S_A .

Using this intuition, we can motivate the solution. Consider the generalization of this picture, where the fluid consists of a continuous series of cylindrical shells each flowing down the pipe and interacting with their neighboring shells. Find a differential relation connecting the velocity of a layer with its radius. Remember the no-slip boundary condition: v ( R ) = 0 v(R) = 0 .

Solve the differential equation and find the velocity of the sap at a distance r r from the center of the tube.

Assumptions

  • There is a pressure Δ p = 1 0 6 \Delta p=10^6 Pa over the pipe
  • r r = 10 μ \mu m
  • The radius of the pipe is 20 μ \mu m
  • The viscosity of the sap is 5 × 1 0 3 5\times 10^{-3} Pa s
  • The length of the pipe is 35 m


The answer is 0.000428571.

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