Critical slot size for deflagration initiation by hot products discharge into hydrogen air-atmospheres

被引:4
作者
Carpio, Jaime [1 ]
Iglesias, Immaculada [2 ]
Vera, Marcos [2 ]
Sanchez, Antonio L. [3 ]
机构
[1] Univ Politecn Madrid, ETS Ingn Ind, Dept Ingn Energet, E-28006 Madrid, Spain
[2] Univ Carlos III Madrid, Dept Ingn Term & Fluidos, Leganes 28911, Spain
[3] Univ Calif San Diego, Dept Mech & Aerosp Engn, 9500 Gilman Dr, La Jolla, CA 92093 USA
关键词
Deflagration initiation; Hydrogen-air mixtures; Hot-jet ignition; Transient jets; Finite element method; TRANSIENT TURBULENT JET; EXPERIMENTAL SAFE GAP; ADAPTIVE ALGORITHM; IGNITION; COMBUSTION; TRANSMISSION; EXPLOSION; MECHANISM;
D O I
10.1016/j.ijhydene.2016.10.010
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
This computational study addresses deflagration initiation of lean, stoichiometric, and moderately rich hydrogen air mixtures by the sudden discharge of a hot planar jet of its adiabatic combustion products. The objective is to determine the minimum slot size required for ignition, a relevant quantity of interest for safety and technological applications concerning the accidental ignition of hydrogen. For sufficiently small jet velocities, the numerical solution of the problem requires integration of the two-dimensional Navier Stokes equations for chemically reacting ideal-gas mixtures, supplemented by standard descriptions of the molecular transport terms and a reduced chemical kinetic mechanism suitable for hydrogen air combustion. The computations provide the variation of the critical slot size for hot-jet ignition with both the jet Reynolds number and the equivalence ratio of the mixture. In particular, it is seen that, while the Reynolds number exerts only a relatively weak effect on the ignition process, the influence of the equivalence ratio is much more pronounced, with the smallest slot widths found for stoichiometric or slightly rich conditions. The numerical results show three different ignition modes, with the flame developing from a clearly identified ignition kernel located either at the core of the leading vortex pair (mode 1), at the symmetry plane near the leading edge of the starting jet (mode 2), or at the jet stem connecting the jet exit with the starting vortex (mode 3). (C) 2016 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:1298 / 1305
页数:8
相关论文
共 46 条
[1]  
[Anonymous], P INT S EXPL HAZ CLA
[2]  
[Anonymous], FIRE SAF J
[3]  
[Anonymous], P INT S EXPL HAZ CLA
[4]  
[Anonymous], P COMBUST I
[5]  
[Anonymous], 6007912003E IEC
[6]   On ignition mechanisms of premixed CH4/air and H2/air using a hot turbulent jet generated by pre-chamber combustion [J].
Biswas, Sayan ;
Tanvir, Saad ;
Wang, Haifeng ;
Qiao, Li .
APPLIED THERMAL ENGINEERING, 2016, 106 :925-937
[7]   An explicit reduced mechanism for H2-air combustion [J].
Boivin, P. ;
Jimenez, C. ;
Sanchez, A. L. ;
Williams, F. A. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2011, 33 :517-523
[8]   Simulation of a supersonic hydrogen-air autoignition-stabilized flame using reduced chemistry [J].
Boivin, Pierre ;
Dauptain, Antoine ;
Jimenez, Carmen ;
Cuenot, Benedicte .
COMBUSTION AND FLAME, 2012, 159 (04) :1779-1790
[9]   Enhanced combustion by jet ignition in a turbocharged cryogenic port fuel injected hydrogen engine [J].
Boretti, Alberto A. ;
Watson, Harry C. .
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2009, 34 (05) :2511-2516
[10]   Using maximum experimental safe gap to select flame arresters [J].
Britton, LG .
PROCESS SAFETY PROGRESS, 2000, 19 (03) :140-145