The evolution of the temperature field during cavity collapse in liquid nitromethane. Part I: Inert case
arXiv:1710.02429 · doi:10.1007/s00193-018-0802-8
Abstract
We study the effect of cavity collapse in non-ideal explosives as a means of controlling their sensitivity. The aim is to understand the origin of localised temperature peaks (hot spots) which play a key role at the early stages of ignition. Thus we perform 2D and 3D numerical simulations of shock induced gas-cavity collapse in nitromethane. Ignition is the result of a complex interplay between fluid dynamics and exothermic chemical reaction. To understand the relative contribution between these two processes we consider in this first part of the work the evolution of the physical system in the absence of chemical reactions. We employ a multi-phase mathematical formulation which accounts for the large density difference across the gas-liquid interface without generating spurious temperature peaks. The mathematical and physical models are validated against experimental, analytic and numerical data. Previous studies identified the impact of the upwind side of the cavity wall to the downwind one as the main reason for the generation of a hot-spot outside of the cavity; this is also observed in this work. However, it is apparent that the topology of the temperature field is more complex than previously thought and additional hot spots locations exist, arising from the generation of Mach stems rather than jet impact. To explain the generation mechanisms and topology of the hot spots we follow the complex wave patterns generated and identify the temperature elevation or reduction generated by each wave. This allows to track each hot spot back to its origins. We show that the highest hot spot temperatures can be more than twice the post-incident shock temperature of the neat material and can thus lead to ignition. By comparing the maximum temperature observed in the domain in 2D and 3D simulations we show that 3D calculations are necessary to avoid belated ignition times in reactive scenarios.
Due to the limitation "The abstract field cannot be longer than 1,920 characters", the abstract appearing here is slightly shorter than the one in the PDF file
Cited by in corpus (7)
- A multi-physics methodology for the simulation of the two-way interaction of reactive flow and elastoplastic structural response
- Meso-resolved simulations of shock-to-detonation transition in nitromethane with air-filled cavities
- The evolution of the temperature field during cavity collapse in liquid nitromethane. Part II: Reactive case
- Mechanisms of shock-induced initiation at micro-scale defects in energetic crystal-binder systems
- Effect of spatial distribution of mesoscale heterogeneities on the shock-to-detonation transition in liquid nitromethane
- Numerical modelling of shock-bubble interactions using a pressure-based algorithm without Riemann solvers
- High-fidelity simulations of shock initiation of an energetic crystal-binder system due to flyer impact