4.7 Article

Laminar burning speed measurement and flame instability study of H2/CO/air mixtures at high temperatures and pressures using a novel multi-shell model

Journal

COMBUSTION AND FLAME
Volume 168, Issue -, Pages 20-31

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.combustflame.2016.03.018

Keywords

Syngas; Laminar burning speed; Flame instability; Schlieren photography; High pressure; Multi-shell

Funding

  1. Qatar National Research Fund (a member of the Qatar Foundation) [NPRP 7-1449-2-523]

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A new differential based multi-shell model has been developed in conjunction with Schlieren photography to measure laminar burning speeds and to investigate flame structures of H-2/CO/air mixtures. The experiments were carried out in two constant volume vessels; one spherical and one cylindrical. Flame instability has been studied using the cylindrical vessel which was installed in a Z-type Schlieren Shadow-graph system equipped with a high speed CMOS camera, capable of taking pictures up to 40,000 frames per second. Flame instabilities such as cracking and wrinkling have been observed during flame propagation and discussed in terms of the hydrodynamic and thermo-diffusive effects. Laminar burning speeds were measured by a novel thermodynamic model using pressure rise during flame propagation in the spherical chamber. Gases in the vessel are divided into two parts; unburned and burned gases. The burned gases are in the center of sphere surrounded by a small preheat zone followed by the unburned gases. The burned gases were divided into multiple shells to determine the temperature gradient precisely. The following energy transfers have been included in the model: Conductive energy loss to the chamber wall and electrodes, energy transfer in the preheat zone, energy transfer between adjacent shells and radiation energy loss from burned gases. The governing equations of unknown variables have been defined by a set of nonlinear ordinary differential equations which were solved using CVODE solver. Power law correlations have been developed for laminar burning speeds of smooth H-2/CO/air flames over a wide range of temperatures (298 K up to 617 K), pressures (from sub-atmospheric up to 5.5 atm), equivalence ratios (0.6-5) and three different hydrogen concentrations of 5%, 10% and 25%, respectively. Experimental burning speeds of H-2/CO/air mixtures have been compared with available measurements as well as computed values obtained by 1D free flame simulations using three chemical kinetics mechanisms. Comparisons show a very good agreement for the conditions which data is available and the predicted results. (C) 2016 The Combustion Institute. Published by Elsevier Inc. All rights reserved.

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