1999
DOI: 10.1098/rspa.1999.0374
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A note on third–order structure functions in turbulence

Abstract: Starting from the Navier-Stokes equation, we rigorously prove that a modied third order structure functionS 3 (r) asymptotically equals 4 r = 3 (is the dissipation rate) in the large Reynolds number limit of Navier-Stokes equation in an inertial regime. From this result, we rigorously conrm the Kolmogorov four-fth law, without the Kolmogorov assumption on isotropy. Our denition of the structure function involves a solid angle averaging over all possible orientation of the displacement v ector y, besides space-… Show more

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Cited by 53 publications
(80 citation statements)
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“…However, while the linear scaling in r of the third-order structure function is fairly robust, the coefficient exhibits only a slow trend toward 4/5 as indicated by the numerical work of [7]. It is clear that for anisotropic forcing, some choices of directions for the vector increment r are more "isotropic" than others [8].…”
Section: Introductionmentioning
confidence: 98%
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“…However, while the linear scaling in r of the third-order structure function is fairly robust, the coefficient exhibits only a slow trend toward 4/5 as indicated by the numerical work of [7]. It is clear that for anisotropic forcing, some choices of directions for the vector increment r are more "isotropic" than others [8].…”
Section: Introductionmentioning
confidence: 98%
“…However, the interpolation of square grid data over spherical shells has been deemed too expensive [8], or, when some such interpolation scheme is implemented, has not been used at sufficiently high Reynolds numbers as will allow for observations of the K41 type [17]. The new angle-averaged and "local" laws of [8,9,10] provide us with the theoretical impetus to investigate and extract the isotropic component of the flow in high-Reynolds number anisotropic turbulence. We use a novel means of taking the average over angles which avoids the expense and effort of interpolating the square-grid data over spherical shells.…”
Section: Introductionmentioning
confidence: 99%
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“…The basic result of (1.1) is that, at sufficiently large Reynolds numbers, an intermediate range of scales exists, away from energy injection and energy dissipation, where the energy flux across scales is identified as δu 3 /r. This expression provides a direct evaluation of the energy cascade through the inertial range (see Nie & Tanveer 1999;Aoyama et al 2005;Gotoh & Watanabe 2005;Ishihara, Gotoh & Kaneda 2009). …”
Section: Introductionmentioning
confidence: 99%