Explosive dispersal of particles in high speed environments

Author:

Durant B. A.1,Garno J.2,Ouellet F.3ORCID,Jackson T. L.1ORCID,Balachandar S.1ORCID,Littrell D.4ORCID

Affiliation:

1. Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, Florida 32611, USA

2. M Division, Los Alamos National Laboratory, Los Alamos, New Mexico 87544, USA

3. X Computational Physics Division, Los Alamos National Laboratory, Los Alamos, New Mexico 87544, USA

4. Air Force Research Laboratory, Munitions Directorate, Eglin Air Force Base, Florida 32542, USA

Abstract

In this paper, we present the results of the explosive dispersal of particles in high-speed environments. We carry out Euler–Lagrange numerical simulations of a source at quiescent ambient conditions as well as moving at Mach numbers of 3 and 6. Particle volume fractions of 0%, 1%, and 4.5% are presented. The detonation profile is computed with the Jones–Wilkins–Lee equation of state using a reactive burn model. Non-static cases provide a framework to consider the effect of a bow shock and pre-existing high-speed flow conditions on the dispersal process. We also compute averages of both static and dynamic pressures, as well as impulse density histories on virtual probe planes to characterize the momentum of the flow and particles that would deposit on a target. Results suggest that the presence of the particles can have a substantial effect on the pressure average of the virtual target planes.

Funder

U.S. Department of Energy

Naval Surface Warfare Center

Publisher

AIP Publishing

Subject

General Physics and Astronomy

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