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The Taylor instability is a secondary flow which occurs as a transition from rotary Couette Flow in the annular gap between two coaxial cylinders of differing diameter when the inner cylinder rotates faster than a critical value. Pairs of counter-rotating axisymmetric (toroidal) vortices are formed in the radial and axial directions while the principal flow continues to be around the azimuth (Figure 1.).

Coaxial cylinder geometry with exploded view of Taylor vortices.

Figure 1. Coaxial cylinder geometry with exploded view of Taylor vortices.

The onset of vortices has been studied experimentally by observing the consequences of their motion: namely to increase the wall shear stress (torque), the rate of heat transfer and the rate of mixing within the fluid. Vortices are generated if the Taylor Number, Ta = ri(ρω/η)2(ro – ri)3 exceeds a critical value, Tac, where ri and ro are the inner and outer radii, respectively, ρ is the fluid density, η the viscosity and ω the rotational speed. The limiting case, ri/ro → 1, was solved theoretically by Taylor to yield Tac,(ri/ro→1)=1695. For long annuli having a small annular gap, , the critical Taylor number may be approximated by Tac = π4(1 + ro/ri)2/(4P) with P = 0.0571(1 – 0.652(ro/ri – 1)) + 0.00056/(1 – 0.652(ro/ri – 1)).

A multitude of higher order instabilities which are non-axisymmetric and time periodic, occur if the Taylor number is increased further. Superimposed Poiseuille Flow, described by a Reynolds Number Re = 2ρu(ro – ri)/η, delays the Taylor instability. Rotation reduces the Reynolds number for transition from laminar to turbulent flow and the combined system is described by a regime map (Figure 2).

Regime map for Taylor vortices in the presence of an axial flow.

Figure 2. Regime map for Taylor vortices in the presence of an axial flow.

Positioning the axis of the inner cylinder a distance, δ, from the axis of the outer cylinder produces an eccentric annulus and causes the Taylor instability to be delayed by an amount dependent on the eccentricity, ε = δ/(ro – ri) and given by Tac(ε) = Tac(1 + 2.6185ε2 + O(ε4)).

The critical Taylor number is also modified by Non-Newtonian Fluid behavior. The theoretical analysis for a Generalized Newtonian fluid characterized by is discussed in Tanner (1985) and the onset of Taylor vortices given by Tac(β) = Tac(l + 0.505β + O(β2)) for ri/ro → 1. The viscosity used in defining the Taylor number for non-Newtonian fluids is η = ; .

REFERENCES

Stuart, J. T. (1986) Taylor-vortex flow: a dynamical system, SIAM Review, 28, 3, 315–342, 1986.

Lockett, T. J. (1992) Numerical Simulation of Inelastic Non-Newtonian Fluid Flows in Annuli, Ph.D. thesis, Imperial College, University of London.

Tanner, R. I. (1985) Engineering Rheology, Clarendon Press, Oxford.

Taylor, G. I. (1923) Stability of a viscous fluid contained between two rotating cylinders, Philosophical Transactions of the Royal Society of London, Series A, Vol. 223, 289–343.

References

  1. Stuart, J. T. (1986) Taylor-vortex flow: a dynamical system, SIAM Review, 28, 3, 315–342, 1986. DOI: 10.1137/1028104
  2. Lockett, T. J. (1992) Numerical Simulation of Inelastic Non-Newtonian Fluid Flows in Annuli, Ph.D. thesis, Imperial College, University of London.
  3. Tanner, R. I. (1985) Engineering Rheology, Clarendon Press, Oxford.
  4. Taylor, G. I. (1923) Stability of a viscous fluid contained between two rotating cylinders, Philosophical Transactions of the Royal Society of London, Series A, Vol. 223, 289–343.
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