Numerical study of premixed flame dynamics in a closed tube: Effect of wall boundary condition

Author: Li, X. X., Xiao, H. H., Duan, Q. L., Sun, J. H.

Journal: Proceedings of the Combustion Institute

DOI: 10.1016/j.proci.2020.08.032

Keywords: Wall boundary condition, Distorted tulip flame, Corrugated flame, Shock-flame interaction, Richtmyer-Meshkov instability, tulip flame, detonation transition, deflagration, evolution, front

Abstract: 

Numerical simulations were conducted to study the dynamics of premixed flames propagating in a closed tube by solving the fully compressible reactive Navier-Stokes equations using a high-order numerical method on a dynamically adapting grid. A simplified chemical-diffusive model was used to describe the reactions and energy release in a stoichiometric hydrogen-air mixture. The influence of wall boundary condition on the flame dynamics was explored by considering three different types of condition on the walls: adiabatic no-slip, adiabatic free-slip, and isothermal. The calculations show that the wall boundary condition has a significant effect on the generation and amplification of pressure waves and consequently on the flame dynamics. In the early stages of flame propagation, the flame behaves in a similar manner for different boundary conditions, that is, the flame develops a tulip shape that further evolves into a distorted tulip flame (DTF) through Rayleigh-Taylor instability arising from acoustic-flame interaction. Significant differences, however, arise after DTF formation in the late stages, especially when the primary acoustic wave is amplified to form a shock wave in the adiabatic free-slip and isothermal cases. The shock-flame interactions facilitate the formation of a series of increasingly corrugated flames by triggering the Richtmyer-Meshkov instabilities. The way how the lateral flame fronts touch the tube sidewalls to generate the primary acoustics and the heat conduction through the tube sidewalls play an important role in the generation and amplification of the pressure waves. (c) 2020 The Combustion Institute. Published by Elsevier Inc. All rights reserved.