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Fernando F. Grinstein

Researcher at Los Alamos National Laboratory

Publications -  152
Citations -  7306

Fernando F. Grinstein is an academic researcher from Los Alamos National Laboratory. The author has contributed to research in topics: Turbulence & Large eddy simulation. The author has an hindex of 36, co-authored 152 publications receiving 6952 citations. Previous affiliations of Fernando F. Grinstein include United States Department of the Navy & United States Naval Research Laboratory.

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Proceedings ArticleDOI

RANS Initialization and Validation in Shock-Driven Turbulent Mixing

TL;DR: A working framework for testing unsteady engineering model initialization and closures based on comparing moments extracted from ensemble-averaged threedimensional large-eddy simulation (LES) data and those predicted directly by a twodimensional, variable-density, compressible, Reynolds-Averaged Navier-Stokes (RANS) model is investigated.
Book ChapterDOI

The Filtering Approach as a Tool for Modeling and Analyzing Turbulence

TL;DR: The Filtering Approach (FA) is a simple multiscale method of analysis, it extends the statistical formalism to a generic filtering operator and main ingredients are the Generalized Central Moments homomorphic to the Statistical Central Moments (SCM), and at present is more and more applied to analyze turbulence and extract statistical data from under-resolved databases as mentioned in this paper.
Posted Content

Effects of Initial Condition Spectral Content on Shock Driven Turbulent Mixing

Abstract: The mixing of materials due to the Richtmyer-Meshkov instability and the ensuing turbulent behavior is of intense interest in a variety of physical systems including inertial confinement fusion, combustion, and the final stages of stellar evolution. Extensive numerical and laboratory studies of shock-driven mixing have demonstrated the rich behavior associated with the onset of turbulence due to the shocks. Here we report on progress in understanding shock-driven mixing at interfaces between fluids of differing densities through 3D numerical simulations using the RAGE code in the implicit large eddy simulation context. We consider a shock tube configuration with a band of high density gas (SF$_6$) embedded in low density gas (air). Shocks with a Mach number of 1.26 are passed through SF$_6$ bands, resulting in transition to turbulence driven by the Richtmyer-Meshkov instability. The system is followed as a rarefaction wave and a reflected secondary shock from the back wall pass through the SF$_6$ band. We apply a variety of initial perturbations to the interfaces between the two fluids in which the physical standard deviation, wave number range, and the spectral slope of the perturbations are held constant, but the number of modes initially present is varied. By thus decreasing the density of initial spectral modes of the interface, we find that we can achieve as much as 25\% less total mixing at late times. This has potential direct implications for the treatment of initial conditions applied to material interfaces in both 3D and reduced dimensionality simulation models.