Laws of turbulence decay from direct numerical simulations

Author:

Panickacheril John John1ORCID,Donzis Diego A.2,Sreenivasan Katepalli R.13ORCID

Affiliation:

1. Department of Mechanical and Aerospace Engineering, New York University, New York, NY 10012, USA

2. Department of Aerospace Engineering, Texas A&M University, College Station, TX 77843, USA

3. Department of Physics and Courant Institute of Mathematical Sciences, New York University, New York, NY 10012, USA

Abstract

Inspection of available data on the decay exponent for the kinetic energy of homogeneous and isotropic turbulence (HIT) shows that it varies by as much as 100%. Measurements and simulations often show no correspondence with theoretical arguments, which are themselves varied. This situation is unsatisfactory given that HIT is a building block of turbulence theory and modelling. We take recourse to a large base of direct numerical simulations and study decaying HIT for a variety of initial conditions. We show that the Kolmogorov decay exponent and the Birkhoff–Saffman decay are both observed, albeit approximately, for long periods of time if the initial conditions are appropriately arranged. We also present, for both cases, other turbulent statistics such as the velocity derivative skewness, energy spectra and dissipation, and show that the decay and growth laws are approximately as expected theoretically, though the wavenumber spectrum near the origin begins to change relatively quickly, suggesting that the invariants do not strictly exist. We comment briefly on why the decay exponent has varied so widely in past experiments and simulations. This article is part of the theme issue ‘Scaling the turbulence edifice (part 1)’.

Funder

US National Science Foundation

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Reference61 articles.

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2. Turbulent Flows

3. Homogeneous, Isotropic Turbulence

4. Modelling Turbulence in Engineering and the Environment

5. Decay of Turbulence at High Reynolds Numbers

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