Shock-induced ignition and transition to detonation in the presence of mechanically induced nonlinear acoustic forcing

We address the problem of shock-induced ignition and transition to detonation in a reactive medium in the presence of mechanically induced fluctuations by a moving oscillating piston. For the inert problem prior to ignition, we provide a novel closed-form model in Lagrangian coordinates for the generation of the train of compression and expansions, their steepening into a train of N-shock waves and their reflection on the lead shock, as well as the distribution of the energy dissipation rate in the induction zone. The model is found to be in excellent agreement with numerics. Reactive calculations were performed for hydrogen and ethylene fuels using a novel high-fidelity scheme to solve the reactive Euler equations written in Lagrangian coordinates. Different regimes of ignition and transition to detonation, controlled by the time scale of the forcing and the two time scales of the chemistry: the induction and reaction times. Two novel hotspot cascade mechanisms were identified. The first relies on the coherence between the sequence of hotspot formation set by the piston forcing and forward-wave interaction with the lead shock, generalising the classic runaway in fast flames. The second hotspot cascade is triggered by the feedback between the pressure pulse generated by the first-generation hotspot cascade and the shock. For slow forcing, the sensitisation is through a modification to the classic runaway process, while the high-frequency regime leads to very localised subcritical hotspot formation controlled by the cumulative energy dissipation of the first-generation shocks at a distance comparable with the shock formation location.

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Publication Details

Journal
Journal of Fluid Mechanics
Published
2025-04-21
DOI
https://doi.org/10.1017/jfm.2025.229
Citations
2
Primary Topic
Combustion and Detonation Processes
Type
article
Field-Weighted Citation Impact
9.99

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article

Shock-induced ignition and transition to detonation in the presence of mechanically induced nonlinear acoustic forcing

Wentian Wang, James G. McDonald, Matei I. Radulescu
2 citations
Journal of Fluid Mechanics
Combustion and Detonation Processes
9.99
article

Shock-induced ignition and transition to detonation in the presence of mechanically induced nonlinear acoustic forcing

Wentian Wang, James G. McDonald, Matei I. Radulescu
article en
2 citations

Abstract

We address the problem of shock-induced ignition and transition to detonation in a reactive medium in the presence of mechanically induced fluctuations by a moving oscillating piston. For the inert problem prior to ignition, we provide a novel closed-form model in Lagrangian coordinates for the generation of the train of compression and expansions, their steepening into a train of N-shock waves and their reflection on the lead shock, as well as the distribution of the energy dissipation rate in the induction zone. The model is found to be in excellent agreement with numerics. Reactive calculations were performed for hydrogen and ethylene fuels using a novel high-fidelity scheme to solve the reactive Euler equations written in Lagrangian coordinates. Different regimes of ignition and transition to detonation, controlled by the time scale of the forcing and the two time scales of the chemistry: the induction and reaction times. Two novel hotspot cascade mechanisms were identified. The first relies on the coherence between the sequence of hotspot formation set by the piston forcing and forward-wave interaction with the lead shock, generalising the classic runaway in fast flames. The second hotspot cascade is triggered by the feedback between the pressure pulse generated by the first-generation hotspot cascade and the shock. For slow forcing, the sensitisation is through a modification to the classic runaway process, while the high-frequency regime leads to very localised subcritical hotspot formation controlled by the cumulative energy dissipation of the first-generation shocks at a distance comparable with the shock formation location.

Journal of Fluid MechanicsVol. 1009
University of Ottawa (CA)
Shell, Natural Sciences and Engineering Research Council of Canada, Air Force Office of Scientific Research
Openalex Percentile: Top 3%
Combustion and Detonation Processes
9.99
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