Geometry and dynamics of passive scalar structures in compressible turbulent mixing

• Published in: Physics of fluids (1994) 2021-10, Vol.33 (10)
• Main Authors: Buchmeier, Jonas, Bußmann, Alexander, Bermejo-Moreno, Iván
• Format: Article
• Language: English
• Subjects: Alignment; Amplification; CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS; Compressibility; Compressive properties; Deformation; Direct numerical simulation; Evolutionary algorithms; Fluid dynamics; Fluid flow; Isotropic turbulence; Mach number; Non Euclidean geometry; Numerical analysis; Physics; Reynolds number; Shock compression; Shock waves; Strain rate; Surface geometry; Turbulent flow; Turbulent flows; Turbulent mixing
• ISSN: 1070-6631; 1089-7666
• DOI: 10.1063/5.0068010

We present a structure-based numerical analysis of passive scalar mixing in decaying homogeneous isotropic turbulence (DHIT) and shock-turbulence interaction canonical configurations. The analysis focuses on the temporal evolution of ensembles of passive scalar structures, initialized as spheres of different sizes relative to the Taylor microscale. An algorithm is introduced to track the evolution of each individual structure and the interactions with other structures in the ensemble, relating changes in the surface geometry and the underlying physical processes (turbulent transport, scalar dissipation, and shock compression). The tracking algorithm is applied to datasets from shock-capturing direct numerical simulations of DHIT, with Taylor microscale Reynolds number R e λ = 40 and turbulence Mach number M t = 0.2, and STI cases in which the turbulence is processed by a shock wave at Mach numbers M = 1.5 and 3.0. Temporal surface convolution increases for initially larger structures, resulting in a higher probability of locally hyperbolic geometries where breakup into smaller structures occurs. Shock-induced deformation of the structures amplifies breakup processes, enhancing mixing, particularly for larger structures. Mixing enhancement by the shock is manifested as an amplification of the surface-averaged scalar gradient, which increases for initially larger structures. The alignment between the scalar gradient and the most extensional strain-rate eigendirection on the scalar isosurfaces also increases across the shock. Larger magnitudes of the scalar gradient and its alignment with the most compressive strain-rate eigendirection correlate with flatter surface regions. Shock-induced structure compression increases the area coverage of flat regions, where the amplification of scalar gradient is localized.