Explosively driven Richtmyer–Meshkov instability jet suppression and enhancement via coupling machine learning and additive manufacturing

Author:

Sterbentz Dane M.1ORCID,Kline Dylan J.1ORCID,White Daniel A.1ORCID,Jekel Charles F.1ORCID,Hennessey Michael P.1ORCID,Amondson David K.1ORCID,Wilson Abigail J.1ORCID,Sevcik Max J.12ORCID,Villena Matthew F. L.1ORCID,Lin Steve S.1,Grapes Michael D.1ORCID,Sullivan Kyle T.1ORCID,Belof Jonathan L.1ORCID

Affiliation:

1. Lawrence Livermore National Laboratory 1 , Livermore, California 94550, USA

2. Colorado School of Mines 2 , Golden, Colorado 80401, USA

Abstract

The ability to control the behavior of fluid instabilities at material interfaces, such as the shock-driven Richtmyer–Meshkov instability, is a grand technological challenge with a broad number of applications ranging from inertial confinement fusion experiments to explosively driven shaped charges. In this work, we use a linear-geometry shaped charge as a means of studying methods for controlling material jetting that results from the Richtmyer–Meshkov instability. A shaped charge produces a high-velocity jet by focusing the energy from the detonation of high explosives. The interaction of the resulting detonation wave with a hollowed cavity lined with a thin metal layer produces the unstable jetting effect. By modifying the characteristics of the detonation wave prior to striking the lined cavity, the kinetic energy of the jet can be enhanced or reduced. Modifying the geometry of the liner material can also be used to alter jetting properties. We apply optimization methods to investigate several design parameterizations for both enhancing or suppressing the shaped-charge jet. This is accomplished using 2D and 3D hydrodynamic simulations to investigate the design space that we consider. We also apply new additive manufacturing methods for producing the shaped-charge assemblies, which allow for the experimental testing of complicated design geometries obtained through computational optimization. We present a direct comparison of our optimized designs with experimental results carried out at the High Explosives Application Facility at Lawrence Livermore National Laboratory.

Funder

Lawrence Livermore National Laboratory

Laboratory Directed Research and Development

Publisher

AIP Publishing

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