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Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets

Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets
Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets
The differences of flow characterization at the different stages of flame acceleration and transition to detonation in tubes with smooth walls, solid obstacles, and fluid jets are studied, especially the effects of flow instabilities on the process. The two-dimensional viscous unsteady reactive Navier–Stokes equations with a detailed chemistry model are solved numerically based on the structured adaptive mesh refinement technique in Adaptive Mesh Refinement Object-oriented C++. During the ignition to a low-speed flame stage, it is found that initial pressure wave interactions with the wall and Rayleigh–Taylor instabilities, induced by the density and pressure gradient misalignment between the ignition region and unburned gas, accelerate the wrinkling and deformation of the flame surface. Consequentially, the flame wrinkles trigger Darrieus–Landau instabilities and as a result the flame accelerates. At the main acceleration stage, the Kelvin–Helmholtz instability formed in the wake of solid obstacles and the strong Kelvin–Helmholtz instability caused by the jets lead to the formation of strong turbulent structures in the flowfield and accelerate the flame propagation. Richtmyer–Meshkov instabilities caused by the interactions of reflected shock waves and the flame surface lead to flame acceleration in the case with solid obstacles. Compared to the tube with fluid jets, although the solid obstacles induce stronger Richtmyer–Meshkov instabilities, the effect of Kelvin–Helmholtz instabilities is not obvious. In general, Darrieus–Landau instabilities and Rayleigh–Taylor instabilities dominate at the initial flame-developing stage, and Kelvin–Helmholtz instabilities and Richtmyer–Meshkov instabilities play a more critical role in the flame acceleration due to interactions of the flame, the shock, solid obstacles, and vortices during the deflagration propagation stage.
1432-2153
617-632
Luan, Zhenye
8cf68510-8da1-4040-9ebc-820bcc311a4c
Huang, Yue
b61d46a7-90a8-4c1f-bd59-de326fc2eb87
Deiterding, Ralf
ce02244b-6651-47e3-8325-2c0a0c9c6314
Peng, Han
62906b46-9628-43fc-921d-b6257b1fec6f
You, Yancheng
e6ecac38-5fd5-4767-9e6c-f7a1b811c59f
Luan, Zhenye
8cf68510-8da1-4040-9ebc-820bcc311a4c
Huang, Yue
b61d46a7-90a8-4c1f-bd59-de326fc2eb87
Deiterding, Ralf
ce02244b-6651-47e3-8325-2c0a0c9c6314
Peng, Han
62906b46-9628-43fc-921d-b6257b1fec6f
You, Yancheng
e6ecac38-5fd5-4767-9e6c-f7a1b811c59f

Luan, Zhenye, Huang, Yue, Deiterding, Ralf, Peng, Han and You, Yancheng (2022) Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets. Shock Waves, 32, 617-632. (doi:10.1007/s00193-022-01100-7).

Record type: Article

Abstract

The differences of flow characterization at the different stages of flame acceleration and transition to detonation in tubes with smooth walls, solid obstacles, and fluid jets are studied, especially the effects of flow instabilities on the process. The two-dimensional viscous unsteady reactive Navier–Stokes equations with a detailed chemistry model are solved numerically based on the structured adaptive mesh refinement technique in Adaptive Mesh Refinement Object-oriented C++. During the ignition to a low-speed flame stage, it is found that initial pressure wave interactions with the wall and Rayleigh–Taylor instabilities, induced by the density and pressure gradient misalignment between the ignition region and unburned gas, accelerate the wrinkling and deformation of the flame surface. Consequentially, the flame wrinkles trigger Darrieus–Landau instabilities and as a result the flame accelerates. At the main acceleration stage, the Kelvin–Helmholtz instability formed in the wake of solid obstacles and the strong Kelvin–Helmholtz instability caused by the jets lead to the formation of strong turbulent structures in the flowfield and accelerate the flame propagation. Richtmyer–Meshkov instabilities caused by the interactions of reflected shock waves and the flame surface lead to flame acceleration in the case with solid obstacles. Compared to the tube with fluid jets, although the solid obstacles induce stronger Richtmyer–Meshkov instabilities, the effect of Kelvin–Helmholtz instabilities is not obvious. In general, Darrieus–Landau instabilities and Rayleigh–Taylor instabilities dominate at the initial flame-developing stage, and Kelvin–Helmholtz instabilities and Richtmyer–Meshkov instabilities play a more critical role in the flame acceleration due to interactions of the flame, the shock, solid obstacles, and vortices during the deflagration propagation stage.

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More information

Accepted/In Press date: 5 March 2021
Published date: 4 November 2022

Identifiers

Local EPrints ID: 477526
URI: http://eprints.soton.ac.uk/id/eprint/477526
ISSN: 1432-2153
PURE UUID: 4e937774-b217-496b-aafc-514e09118c48
ORCID for Ralf Deiterding: ORCID iD orcid.org/0000-0003-4776-8183
ORCID for Han Peng: ORCID iD orcid.org/0000-0003-4503-360X

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Date deposited: 07 Jun 2023 17:14
Last modified: 17 Mar 2024 03:58

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Contributors

Author: Zhenye Luan
Author: Yue Huang
Author: Ralf Deiterding ORCID iD
Author: Han Peng ORCID iD
Author: Yancheng You

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