Coaxial Cylinders Flow: Examining Velocity & Stress in a Rotating Fluid

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SUMMARY

The discussion focuses on the flow of an incompressible fluid between two coaxial cylinders, with the outer cylinder rotating at angular velocity w. The azimuthal velocity component, vφ, is derived from the differential equation d²vφ/dr² + (1/r)(dvφ/dr) - vφ/r² = 0. The stress tensor in the fluid is calculated, and the moment about the axis of rotation of the frictional forces acting on each cylinder is obtained. This analysis is crucial for understanding fluid dynamics in biomedical engineering applications.

PREREQUISITES
  • Understanding of fluid dynamics principles
  • Familiarity with the Navier-Stokes equations in cylindrical coordinates
  • Knowledge of stress tensor calculations in fluid mechanics
  • Basic concepts of angular velocity and its effects on fluid flow
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  • Study the derivation of the Navier-Stokes equations in cylindrical coordinates
  • Learn about stress tensor analysis in fluid mechanics
  • Research the implications of angular velocity on fluid behavior in rotating systems
  • Explore applications of coaxial cylinder flow in biomedical engineering
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Biomedical engineering students, fluid dynamics researchers, and professionals involved in the design of rotating systems in medical devices.

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A real incompressible fluid is contained in the region between two coaxial cylinders of radii R1 and R2. The outsider cylinder rotates with angular velocity w, in stationary regime, and the flow is purely circular. Neglect the action of gravity.

a) Show that vφ (azimuthal velocity component) obeys the differential equation:

d2vφ/dr2 + (1/r) . (dvφ/dr) - vφ/r2 = (d/dr). [(1/r). (d/dr)(rvφ)] = 0

and determine vφ.b) Calculate the stress tensor in the fluid;

c) Obtain the moment about the axis of rotation of the frictional forces in each of the cylinders;

Thank you so much for your attention. I'm studying biomedical engineering and I have a biomechanics exam tomorrow and I'm really in trouble. I'd be very thankfull if someone could help me.
 

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Start out with the theta component of the Navier stokes equations in cylindrical coordinates. The inertial terms, the pressure term, and the gravitational term are going to be zero for your problem. This leaves only the viscous term. The viscous term leads to the equation you gave.

Chet
 

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