1979
DOI: 10.1103/physrevb.20.2690
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Temperature and velocity dependence of superfluid turbulence

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Cited by 39 publications
(26 citation statements)
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“…Griffiths [20] showed an increase of v sc up to 1.9 K, whereas Jones described a dependence on the superfluid density, thus decreasing as the temperature approaches T λ [21]. [17] is also reported. Note that the cross section of sample 3 is unknown, therefore we have used the one obtained with the above reported Landau's analysis.…”
Section: Critical Heat Flux Identifying the End Of The Landau Regime mentioning
confidence: 99%
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“…Griffiths [20] showed an increase of v sc up to 1.9 K, whereas Jones described a dependence on the superfluid density, thus decreasing as the temperature approaches T λ [21]. [17] is also reported. Note that the cross section of sample 3 is unknown, therefore we have used the one obtained with the above reported Landau's analysis.…”
Section: Critical Heat Flux Identifying the End Of The Landau Regime mentioning
confidence: 99%
“…As observed in the previous sub-section, at 2.0 K the transition between laminar and turbulent regime is not always as sharp as for lower bath temperatures [16], thus making difficult to estimate Q c1 . FIGURE 6 also reports Q c1 values predicted by Ladner and Tough [17] in the case of our geometries. They are in rather good agreement with those of sample 2 until the peak at 1.9 K, despite the geometrical and fitting parameters present in [16] that are not known in our case.…”
Section: Critical Heat Flux Identifying the End Of The Landau Regime mentioning
confidence: 99%
“…Inspiring in the so-called phonon hydrodynamics in the rarefied regime, one admits a heat flux slip flow along the walls, instead of the non slip condition. For this reason we choose (17) q w = −C ∂q(y, z) ∂z z=b where C is a non-negative parameter, which in kinetic theory of rarefied gases ma be identified as C = 2 − f f [4,6]. More arguments on the interesting subject of no-slip condition can be find in Ref.…”
Section: Equation and Heat Profilementioning
confidence: 99%
“…It must be said that, furthermore, the transition between the laminar and the turbulent regime is very complicated, so that between (1) and (3) there is a considerable range of intermediate states not yet completely described. The rectangular tube was not fully studied in this situation apart from the paper by Ladner and Tough [17]. 3.…”
Section: Introductionmentioning
confidence: 99%
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