2009
DOI: 10.1016/j.ijhydene.2009.08.054
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Spherical expanding flames in H2–N2O–Ar mixtures: flame speed measurements and kinetic modeling

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Cited by 57 publications
(47 citation statements)
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“…The detailed model can also be used to predict laminar flame speeds for H 2 -N 2 O-Ar mixtures as shown in [33,53]. Through this extensive validation, the present detailed kinetic mechanism for H 2 -N 2 O mixtures is suitable for the modeling of a wide range of combustion events and initial conditions.…”
Section: Kinetic Scheme Validationmentioning
confidence: 92%
See 1 more Smart Citation
“…The detailed model can also be used to predict laminar flame speeds for H 2 -N 2 O-Ar mixtures as shown in [33,53]. Through this extensive validation, the present detailed kinetic mechanism for H 2 -N 2 O mixtures is suitable for the modeling of a wide range of combustion events and initial conditions.…”
Section: Kinetic Scheme Validationmentioning
confidence: 92%
“…Previous studies on hydrogen-nitrous oxide mixtures have generated data sets on the ignition delay time [15,16,17,18,19,20,21,22,23,24,25,26], the laminar burning speed [27,28,29,30,31,32,33,34,35], and the minimum ignition energy [36]. Concerning detonation, Zhang et al measured the critical energy for direct initiation [37] and the cell sizes have been measured [38,39] in the frame work of nuclear waste storage risk assessment.…”
Section: Introductionmentioning
confidence: 99%
“…To investigate these processes at a more fundamental level, a number of studies involving the pyrolysis of N2O and the oxidation of hydrogen/NOx and syngas/NOx have been performed in shock tubes [8,[16][17][18][19][20][21][22][23][24][25][26][27], jet-stirred reactors (JSR) [28][29][30], flow reactors (FR) [9,10,31,32] and spherical expanding laminar flames [33,34]. Simultaneously, many relative kinetic mechanisms [9,10,13,28,32,[35][36][37][38][39][40][41][42][43] have also been proposed to improve our understanding of NOx formation and to develop NOx control strategies.…”
Section: Introductionmentioning
confidence: 99%
“…The mean distance D d-d is then comparable to the flame thickness, d L , estimated based on the H 2 diffusion coefficient, D H2 and the laminar flame speed S L°( d L = D H2 /S L°) . Since S L°c annot be measured close to the downward limit (9%H 2 ), it has been estimated using COSILAB [31] with the detailed mechanism of Mével et al [32]. In these conditions the adiabatic flame temperature was 1243 K, S L°w as 4.2 cm/s leading to a flame thickness d L = 0.7 mm.…”
Section: H 2 /Air/water Mistmentioning
confidence: 99%
“…The s 0 L were calculated by using COSILAB code [31] with kinetic model of Mével et al [32]. The flame speed was estimated by multiplying s 0 L by the expansion coefficient r. The different values are summarized in Table S3 in Supplement.…”
Section: Isolated Droplet and Laminar Flamementioning
confidence: 99%