4.4 Article

A Computer Model to Study the Response of Energetic Materials to a Range of Dynamic Loads

Journal

PROPELLANTS EXPLOSIVES PYROTECHNICS
Volume 43, Issue 7, Pages 703-720

Publisher

WILEY-V C H VERLAG GMBH
DOI: 10.1002/prep.201700287

Keywords

non-shock ignition; strength model; delayed detonation; deflagration; HERMES model

Funding

  1. Joint US DoD/DOE Munitions Technology Development Program
  2. U.S. Department of Energy, National Nuclear Security Administration [DE-AC52-07NA27344, LLNL-JRNL-742811]

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Over the past decade we developed a model to enable computer simulation of the mechanical and subsequent energetic response of explosives and propellants to mechanical insults such as impacts, perforations, drops, and falls. The model is embedded in computer simulation programs that solve the non-linear, large deformation equations of compressible solid and fluid flow in space and time. It is implemented as a user-defined model, which returns the updated stress tensor and composition that result from the simulation supplied strain tensor change. Although it is multi-phase, in that gas and solid species are present, it is single-velocity, in that the gas does not flow through the porous solid. More than 70 time-dependent variables are made available for additional analyses and plotting. The model encompasses a broad range of possible responses: mechanical damage with no energetic response, and a continuous spectrum of degrees of violence including delayed and prompt detonation. This paper describes the basic workings of the model.

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