Optimal Taylor–Couette flow: direct numerical simulations
We numerically simulate turbulent Taylor–Couette flow for independently rotating inner and outer cylinders, focusing on the analogy with turbulent Rayleigh–Bénard flow. Reynolds numbers of $R{e}_{i} = 8\times 1{0}^{3} $ and $R{e}_{o} = \pm 4\times 1{0}^{3} $ of the inner and outer cylinders, respect...
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Veröffentlicht in: | Journal of fluid mechanics 2013-03, Vol.719, p.14-46 |
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Format: | Artikel |
Sprache: | eng |
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Zusammenfassung: | We numerically simulate turbulent Taylor–Couette flow for independently rotating inner and outer cylinders, focusing on the analogy with turbulent Rayleigh–Bénard flow. Reynolds numbers of
$R{e}_{i} = 8\times 1{0}^{3} $
and
$R{e}_{o} = \pm 4\times 1{0}^{3} $
of the inner and outer cylinders, respectively, are reached, corresponding to Taylor numbers
$Ta$
up to
$1{0}^{8} $
. Effective scaling laws for the torque and other system responses are found. Recent experiments with the Twente Turbulent Taylor–Couette (
${T}^{3} C$
) setup and with a similar facility in Maryland at very high Reynolds numbers have revealed an optimum transport at a certain non-zero rotation rate ratio
$a= - {\omega }_{o} / {\omega }_{i} $
of about
${a}_{\mathit{opt}} = 0. 33$
. For large enough
$Ta$
in the numerically accessible range we also find such an optimum transport at non-zero counter-rotation. The position of this maximum is found to shift with the driving, reaching a maximum of
${a}_{\mathit{opt}} = 0. 15$
for
$Ta= 2. 5\times 1{0}^{7} $
. An explanation for this shift is elucidated, consistent with the experimental result that
${a}_{\mathit{opt}} $
becomes approximately independent of the driving strength for large enough Reynolds numbers. We furthermore numerically calculate the angular velocity profiles and visualize the different flow structures for the various regimes. By writing the equations in a frame co-rotating with the outer cylinder a link is found between the local angular velocity profiles and the global transport quantities. |
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ISSN: | 0022-1120 1469-7645 |
DOI: | 10.1017/jfm.2012.596 |