4.7 Article

Properties of turbulent channel flow similarity solutions

期刊

JOURNAL OF FLUID MECHANICS
卷 915, 期 -, 页码 -

出版社

CAMBRIDGE UNIV PRESS
DOI: 10.1017/jfm.2021.132

关键词

shear layer turbulence; turbulent boundary layers; turbulence theory

资金

  1. Australian Research Council [DP170103464]
  2. U.S. Office of Naval Research [N000141712307]
  3. U.S. Department of Defense (DOD) [N000141712307] Funding Source: U.S. Department of Defense (DOD)

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High resolution direct numerical simulation data are used to investigate the similarity solutions for mean velocity and Reynolds shear stress in turbulent channel flow. The analysis yields an invariant form of the mean momentum equation valid over a significant portion of the flow domain. The results provide insights into the development of wall-flow models and support conjectures regarding the behavior of similarity parameters at large Reynolds numbers.
High resolution direct numerical simulation (DNS) data are used to investigate properties of similarity solutions for the mean velocity (U) and Reynolds shear stress (T) in turbulent channel flow. The analysis uses the method of Fife et al. (Multiscale Model. Simul., vol. 4, 2005, p. 936) for determining the asymptotic scaling properties of indeterminate equations. Subject to its primary assumption, the analysis yields an invariant form of the mean momentum equation that is valid over a significant portion of the flow domain. Because the requisite coordinate transformations yield a self-similar relationship between scaled wall-normal derivatives of U and T, this procedure inherently closes the mean equation. These transformations incorporate use of the so-called Fife similarity parameter, phi. The asymptotic constancy of phi (-> phi(c)) on the inertial sublayer is analytically related to the von Karman constant by kappa = phi(-2)(c). Integrations of the transformed mean equation are shown to independently yield similarity solutions for both U and T, and the veracity of these solutions is examined in detail. DNS data at delta(+) similar or equal to 8000 reveal that the primary assumption of the analysis is satisfied to within a deviation of less than 0.1%. The present solutions and their associated similarity structure are further used to generate a number of new results. These include a cogent specification for the both the inner and outer boundaries of the inertial sublayer and a variety of well-founded ways to estimate phi(c) at finite Reynolds number. Extensions of the analytical arguments by Klewicki et al. (Phys. Rev. E, vol. 90, 2014, 063015) support the conjecture that phi(c) -> Phi = (1 + root 5)/2 (or equivalently, kappa = 2/(3 + root 5)) at large Reynolds number. Connections between the channel solutions and those in the other canonical wall flows are briefly discussed, as are potential implications of the present results relative to wall-flow model development.

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