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Our reference: HE 10552 P-authorquery-v9
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Article Number: 10552
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Highlights
< Three ignition regimes are identified according to hydrogen fraction. < Simulated ignition delays using four models were
compared to experimental data. < At high temperature, ignition delay mainly is governed by chain branching reaction. < At
middle-low temperature, HO2 and H2O2 chemistries affect ignition delay.
Available online at www.sciencedirect.com
journal homepage: www.elsevier .com/locate/he
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Please cite this article in press as: ZhangY, et al., Experimental andmodeling study on auto-ignition characteristics ofmethane/hydrogen blends under engine relevant pressure, International Journal of Hydrogen Energy (2012), http://dx.doi.org/10.1016/j.ijhydene.2012.09.056
0360-3199/$ e see front matter Copyright ª 2012, Hydrogen Energy Publications, LLC. Published by Elsevier Ltd. All rights reserved.http://dx.doi.org/10.1016/j.ijhydene.2012.09.056
Experimental and modeling study on auto-ignitioncharacteristics of methane/hydrogen blends under enginerelevant pressure
Q1 Yingjia Zhang, Xue Jiang, Liangjie Wei, Jiaxiang Zhang, Chenglong Tang, Zuohua Huang*
State Key Laboratory of Multiphase Flow in Power Engineering, Xi’an Jiaotong University, Xi’an 710049, China
a r t i c l e i n f o
Article history:
Received 24 April 2012
Received in revised form
25 August 2012
Accepted 9 September 2012
Available online xxx
Keywords:
Shock tube
Methane
Hydrogen
Ignition delay
Sensitivity analysis
a b s t r a c t
Auto-ignition characteristics of methane/hydrogen mixtures with hydrogen mole fraction
varying from 0 to 100% were experimentally studied using a shock tube. Test pressure is
kept 1.8 MPa and temperatures behind reflected shock waves are in the range of 900
e1750 K and equivalence ratios from 0.5 to 2.0. Three ignition regimes are identified
according to hydrogen fraction. They are, methane chemistry dominating ignition ðXH2 �40%Þ, combined chemistry of methane and hydrogen dominating ignition ðXH2 ¼ 60%Þ, andhydrogen chemistry dominating ignition ðXH2 � 80%Þ. Simulated ignition delays using four
models including USC Mech 2.0, GRI Mech 3.0, UBC Mech 2.1 and NUI Galway Mech were
compared to the experimental data. Results show that USC Mech 2.0 gives the best
prediction on ignition delays and it was selected to conduct sensitivity analysis for three
typical methane/hydrogen mixtures at different temperatures. The results suggest that at
high temperature, ignition delay mainly is governed by chain branching reaction
H þ O2 5 OH þ O, and thus increasing equivalence ratio inhibits ignition of methane/
hydrogen mixtures. At middle-low temperature, contribution of equivalence ratio on
ignition delay of methane/hydrogen mixtures is mainly due to chemistries of HO2 and H2O2
radicals.
Copyright ª 2012, Hydrogen Energy Publications, LLC. Published by Elsevier Ltd. All rights
reserved.
1. Introduction
With increased demand on energy and further strengthened
vehicle emission regulation adoption, the mixtures of
methane, the primary composition of natural gas, and
hydrogenwill become one of most promising alternative fuels
due to large reserve in natural gas, and clean combustion
through hydrogen enrichment [1,2]. Many researches have
been conducted in the practical combustion facilities, like IC
engines [3,4] and aerospace [5]. Meanwhile, the fundamental
combustion researches were made, like flame speed
measurements [6e8] and species concentration profile [9,10].
The ratios of methane and hydrogen sometimes vary due
to different supplying and use in different combustion facili-
ties. Different fractions of hydrogen can influence the ignition
and combustion chemistry of methane-hydrogen fuel blend,
and influence the safety and performance in the particular
combustion device. Thus, understanding the ignition kinetics
of methane/hydrogen mixtures will optimize the operation of
the combustion device and avoid the possible faults occurring,
such as knocking, flashback and unstable combustion.
* Corresponding author. Tel.: þ86 29 82665075; fax: þ86 29 82668789.E-mail address: [email protected] (Z. Huang).
Available online at www.sciencedirect.com
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Please cite this article in press as: ZhangY, et al., Experimental andmodeling study on auto-ignition characteristics ofmethane/hydrogen blends under engine relevant pressure, International Journal of Hydrogen Energy (2012), http://dx.doi.org/10.1016/j.ijhydene.2012.09.056
0360-3199/$ e see front matter Copyright ª 2012, Hydrogen Energy Publications, LLC. Published by Elsevier Ltd. All rights reserved.http://dx.doi.org/10.1016/j.ijhydene.2012.09.056
As the fundamental combustion data are hard to obtain in
the practical combustion device, thus, these fundamental
data are usually measured using the standard facilities, such
as shock tube. Lifshitz et al. [11] first experimentally investi-
gated the ignition of methane/hydrogen mixtures using
a shock tube. Cheng and Oppenheim [12] investigated ignition
characteristics of methane/hydrogen mixtures. Recently,
some scholars also reported the ignition characteristics of
methane/hydrogen mixtures [13e19].
In reviewing the literature, it is clear that only limited
studies are available for the ignition delays of methane/
hydrogen at engine relevant pressure, and the fractions of
hydrogen in fuel are also limited in these studies. Meanwhile,
providing sufficient ignition delays can develop and modify
the mechanisms of methane/hydrogen mixtures. For this
purpose, the detailed ignition delays of methane/hydrogen
mixtures were measured in a high-pressure shock tube at
engine relevant pressure, and the effects of equivalence ratio
on ignition of methane/hydrogen mixtures were analyzed. In
addition, normalized sensitivity analysis was made using the
USC Mech 2.0 mechanism [20] to identify key elementary
reactions in the ignition chemistry of methane/hydrogen
mixtures.
2. Experimental setup and procedure
2.1. Experimental setup
Experiments were made in a high-pressure stainless shock
tubewitha115mminnerdiameter. This shock tube facilityhas
been fully described in the previous studies [18,19]. A double
diaphragm machine separates the shock tube into a 4-m long
driver section and a 5.3-m long driven section, as shown in
Fig. 1. In order to measure longer ignition delays at relatively
low temperatures, the tailored interface method was used
through tuning the thermodynamics properties of the driver
gases using different mixtures of helium and nitrogen. Four
fast-response piezoelectric pressure transducers are installed
at fixed intervals along the driven section and three time-
interval counters are used to measure incident shock velocity
with typical attenuation value from 1.8 to 3.2%/m. The test
temperature behind the reflected shock wave is determined
fromthe incident shockvelocitybyusing chemical equilibrium
software GASEQ [21]. Uncertainty of reflected shock tempera-
ture is calculated using a standard error analysis procedure
[22]. In this study, at the reflected shock temperature of 1450 K
and950K, theestimatederrorsare approximately20Kand10K
respectively. The test mixtures were prepared in a 128 L
stainless steel tank according to Dalton’s law of partial pres-
sure andwere kept over 12 h to ensure a sufficientmixing. The
purities of methane, hydrogen, oxygen, nitrogen and helium
are 99.995%, 99.999%, 99.995%, 99.995%, and 99.999%, respec-
tively. When the driven section is evacuated to an ultimate
pressure below 1.0� 10�7 MPa, the test mixtures are filled into
it, and the double diaphragmsare brokenwithin a fewminutes
afterfilling.ThermodynamicdatabaseofUSCMech2.0 [20]was
used in the study. Vibrational relaxation is neglected due to
small amounts of diatomic and polyatomic molecules in this
work.
The reflected shock pressure was traced by a piezoelectric
pressure transducer with acceleration compensation located
at 20 mm from the end-wall of shock tube. Chem-
iluminescence emission from OH* radicals near 307 nm was
detected by a photomultiplier with a narrow band pass filter.
Ignition of the mixtures was monitored by the reflected shock
pressure and OH* emission. The definition of ignition delay is
consistent with Ref. [18]. Typical pressure rise rate (dp/
dt ¼ 4%/ms) from boundary layer effect (i.e. BL effect) is
observed in this study.
2.2. Numerical simulation
Calculated ignition delays and sensitivity analysis of the
methane/hydrogenmixtures were made using the CHEMKINⅡ
[23] program with extensively incorporating the SENKIN [24]
package. In general, for high-temperature (s < 1.5 ms), the
ideal assumption of constant volume (constantU, V) and zero-
Fig. 1 e Schematic of the high-pressure shock tube.
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dimensional model (ZOAM) is reasonable for calculating
ignition delay. For the middle-low temperature (s > 1.5 ms),
however the BL effect becomes important and the dp/dt needs
to be considered in simulation. Therefore, an improved
assumption of constant U, V is used to calculate the ignition
delay of the methane/hydrogen mixtures. Fig. 2 gives
a comparison on the ignition delays between the calculated by
using both methods (i.e. ideal constant U, V and the improved
constant U, V) and measured. Whether methane or hydrogen,
both assumptions are highly consistent with the current data
when s < 1.5 ms. However, an obvious discrepancy is pre-
sented when s > 1.5 ms. Compared to improved constant U, V,
the ideal constant U, V over-predicts the ignition delay in
a factor of 3 for methane at T ¼ 1250 K and a factor of 3 for
hydrogen at T ¼ 1000 K. The related research was reported by
Pang et al. [25].
3. Experimental results and discussion
18 kinds of methane/hydrogen mixtures were tested and
detailed compositions are given in Table 1. The measured
ignition delays of methane/hydrogen are given in Figs. 3e5. de Vries and Petersen [13] and Huang et al. [14] suggested that
certain hydrogen addition ðXH2 < 40%Þ to methane did not
change dominant kinetic of the methane oxidation. The
ignition characteristics of the methane/hydrogen mixtures
were classified into three ignition regimes based on hydrogen
fractions proposed in Ref. [18], i.e. methane chemistry domi-
nating ignition (MCDI), combined chemistry of methane and
hydrogen dominating ignition (CCMHDI) and hydrogen
chemistry dominating ignition (HCDI). Furthermore, two
ignition temperature regions were identified from changing in
global activation energy using a dotted separating line.
3.1. Reaction system in MCDI mixtures
For XH2 � 40% in fuel, the effects from equivalence ratio on
ignition delays are shown in Fig. 3. At high-temperature
region, the ignition delays increase with the increase in
equivalence ratio. Here, ignition kinetic depends on oxygen
concentration in fuel blends. Oxygen concentration increases
with the decrease in equivalence ratio, which increases the
reaction rate of chain branching reaction H þ O2 5 OH þ O
which plays a dominant role at high temperature and
promotes the ignition. Note that the ignition delays increase
slightly for the leanmixtures and increase significantly for the
rich mixture with the increase in equivalence ratio when
XH2 ¼ 40%. The non-linear relationship between logarithmic
of ignition delay and equivalence ratio appears and becomes
obvious with increasing hydrogen fraction.
At middle-low temperature region, the ignition delays still
increase with increasing the equivalence ratio. But the reason
is different to that at high-temperature region. The ignition
kinetics of methane/hydrogen mixtures depends largely on
fuel concentration rather than oxygen concentration. Fuel
concentration increases with the increase in equivalence
ratio, which increases production rate of CH3 and promotes
reaction rate of the chain termination reaction
CH3 þ CH3(þM) 5 C2H6(þM), and then increases the ignition
delays.
Fig. 2 e Comparison of ignition delay calculated by using
both ideal U, V and improved U, V to experiments. (a)
Ignition delay for methane, (b) Ignition delay for hydrogen.
Table 1 e Composition of the test mixtures in the study( p [ 1.8 MPa for all mixtures).
Fuel blends XCH4=ð%Þ XH2=ð%Þ XO2=ð%Þ XAr/(%) f
100%CH4 0.998 0 3.990 95.012 0.5
1.900 0 3.801 94.299 1.0
3.471 0 3.471 93.058 2.0
80%CH4/20%H2 0.931 0.233 3.956 94.880 0.5
1.759 0.440 3.738 94.063 1.0
3.170 0.792 3.368 92.670 2.0
60%CH4/40%H2 0.837 0.558 3.907 94.698 0.5
1.565 1.043 3.652 93.740 1.0
2.769 1.846 3.231 92.154 2.0
40%CH4/60%H2 0.697 1.046 3.834 94.423 0.5
1.282 1.924 3.527 93.267 1.0
2.211 3.316 3.309 91.434 2.0
20%CH4/80%H2 0.464 1.856 3.713 93.967 0.5
0.832 3.327 3.327 92.515 1.0
1.377 5.508 2.754 90.361 2.0
0%CH4 0 3.471 3.471 93.058 0.5
0 5.915 2.958 91.127 1.0
0 9.130 2.283 88.587 2.0
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3.2. Reaction system in CCMHDI mixture
For the 40%CH4/60%H2 mixture, the effect of equivalence ratio
on the ignition delays is shown in Fig. 4. At high-temperature
region, the ignition delays of the mixture increase with the
increase in equivalence ratio like that of MCDI mixture. The
non-linear relationship between logarithmic of the ignition
delay and equivalence ratio becomes more obvious.
At middle-low temperature region, the ignition delays are
insensitive to the variation of equivalence ratio. Here, it is
Fig. 3 e Effects of equivalence ratio on ignition for methane
dominating ignition. (a) 100%CH4, (b) 80%CH4/20%H2, (c)
60%CH4/40H2.
Fig. 4 e Effects of equivalence ratio on ignition delay of
hydrogen and methane dominating mixture.
Fig. 5 e Effects of equivalence ratio on ignition for hydrogen
dominating ignition. (a) 20%CH4/80%H2, (b) 100%H2.
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hard to know whether a single chemistry is dominant or both
chemistries are the balance competition in the ignition kinetic
of CCMHDI mixture. Furthermore, the chemistries of HO2 and
H2O2 become very important for ignition of the methane/
hydrogen mixture at low temperature. A detailed kinetic
analysis will be discussed in Section 4.2.2.
3.3. Reaction system in HCDI mixtures
Fig. 5 shows influence of equivalence ratio on the ignition
delays for hydrogen chemistry dominating. For the 20%CH4/
80%H2 mixture as shown in Fig. 5(a), at high-temperature
region, the results show that a negligible influence from
equivalence ratio is presented at T > 1350 K, and the shortest
ignition delay is given for f¼ 0.5 and the longest ignition delay
is appeared for f ¼ 2.0 at 1220 K < T < 1350 K, and the ignition
delays are close to each other at 1160 K < T < 1220 K. This
reason is the discrepancy from inhibited effect of methane on
ignition at different conditions. At middle-low temperature
region, the ignition delay is insensitive to equivalence ratio.
For pure hydrogen, at high-temperature region, a complex
dependence of ignition delay on equivalence ratio is pre-
sented in Fig. 5(b). The longest ignition delay is given at
f ¼ 0.5, and the shortest one at f ¼ 1.0. At f � 1.0, the
hydrogen concentration increases with the increase in
equivalence ratio which increases the H and OH radicals
through the reaction O þ H2 5 H þ OH, and then promotes
the rate of reaction H þ O2 5 OH þ O. Furthermore, enthalpy
of the mixture increases with increasing hydrogen concen-
tration which increases reaction system temperature. Thus,
the rates of above two endothermic reactions are further
promoted and decrease the ignition delays. At f � 1.0, the
oxygen concentration decreases with the increase in equiv-
alence ratio which decreases the rate of reaction
H þ O2 5 OH þ O, and decreases rate of total reaction and
ignition delays. At middle-low temperature region, the effect
of equivalence ratio on ignition delays is consistent to that at
high-temperature region, and the stoichiometric mixture
gives the shortest ignition delay. Here, the chain termination
reaction H þ O2(þM) 5 HO2(þM) dominates the ignition
kinetic instead of the reaction H þ O2 5 OH þ O. At f � 1.0,
the oxygen concentration decreases with the increase in
equivalence ratio which decreases the rate of reaction
H þ O2(þM) 5 HO2(þM), and then promotes rate of total
reaction and reduces ignition delays. At f � 1.0, the rates of
reaction O þ H2 5 H þ OH and H þ O2(þM) 5 HO2(þM) are
increased as increasing hydrogen concentration and
decreasing oxygen concentration with the increase in equiv-
alence ratio. This inhibits rate of total reaction and increases
the ignition delay.
4. Numerical predictions and comparisonwith experiments
The calculated ignition delays of the methane/hydrogen
mixtures have large discrepancy using different kinetic
models due to different species and rates of elementary reac-
tions in these models. Therefore, the comparison on ignition
delay predicted among different models is necessary for
selecting a reasonable kinetic model in predicting the ignition
delays of the methane/hydrogen mixtures and making sensi-
tivity analysis under the experimental conditions.
4.1. Mechanism selection
Gersen et al. [15] suggested that if a model could well predict
the ignition delays for pure hydrogen and pure methane, this
mechanism could also give reasonable prediction in ignition
delays for methane/hydrogen fuel blends. The view had been
verified by Huang et al. [14] and Zhang et al. [18]. Comparisons
of the calculated ignition delays by using four mechanisms
USCMech 2.0 [20], GRIMech 3.0 [26], UBCMech 2.1 [14] andNUI
Galway Mech [27] with measured ignition delays of methane
and hydrogen are shown in Figs. 6 and 7. For pure methane
mixture, the four models can well predict the ignition delays.
For pure hydrogen mixture, however the models can well
predict the “S” structure except the UBC Mech 2.1 [12]. The
result is not surprising because the hydrogen submodel in
UBC Mech 2.1 [14] is mainly based on GRI Mech 1.2 [28]. It is
well known that the hydrogen submodel in GRI Mech 1.2 [28]
has been only validated by the experimental data at low
pressure and high temperature, but not is optimized by
those data at high pressure and middle-low temperature.
Huang et al. [14] modified the rate coefficients of several
reactions key to hydrogen ignition including the reactions
H þ O2 þ M ¼ HO2 þ M, OH þ H2 ¼ O þ H2O and
H þ O2 þ N2 ¼ HO2 þ N2, nevertheless the equally important
elementary reactions such as HO2 þ HO2 5 O2 þ H2O2 and
OH þ HO2 5 H2O þ O2 are not improved in UBC Mech 2.1 [14].
It is noteworthy that all kinetic models over-predict the igni-
tion delays at middle-low temperature (T < 1000 K), especially
for stoichiometric mixture. This suggests that the current
hydrogen model needs further to be modified at higher pres-
sure and middle-low temperature.
Through the above comparative analyses, the USC Mech
2.0 [20] was selected to calculate the ignition delays of the
methane/hydrogen mixtures and make normalized sensi-
tivity analysis. This model was developed on the basis of GRI
Fig. 6 e Measured and calculated ignition delays for
methane using different kinetic models.
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Mech 1.2 [28] and GRI Mech 3.0 [26], including the optimized
reaction model of H2/CO combustion of Davis et al. [29], the
detailed C2 fuel combustionmodel of Wang and Laskin [30] on
the basis of C2H4 and C2H2 chemistries, the detailed C3 fuel
combustionmodel of Davis et al. [31] on the basis of chemistry
of C3H6 decomposition and oxidation, and the C4 combustion
model of Laskin et al. [32] on the basis of 1, 3-butadiene
oxidation chemistry. This detailed kinetic model includes
111 species and 784 reactions, and was validated by lots of
experimental data, like ignition delays, species concentration
profiles and laminar flame speeds. Furthermore, the rates of
following reactions
HO2 þ HO2 5 O2 þ H2O2 (R18eR19)
OH þ HO2 5 H2O þ O2 (R20eR24)
CO þ OH 5 CO2 þ H (R31eR32)
CO þ HO2 5 CO2 þ OH (R34)
weremodified in their studies, and rates of several C1 and C2
reactionswere re-evaluated. The oxidationmodels of benzene
and toluene are added to the USC Mech 2.0 [20].
4.2. Sensitivity analysis
Sensitivity analysis is used to identify key promotion and/or
inhibition reactions in the ignition process of combustible
mixture, and it will help to further understand the ignition
chemical kinetic. The normalized sensitivity analysis was
conducted for three typical methane/hydrogen mixtures to
study the effects of equivalence ratio on ignition delay at
different temperatures (1400 K and 930 K) and 1.8 MPa using
the USCMech 2.0 [20] in this study. The normalized sensitivity
coefficient is defined as follows,
S ¼ sð2:0kiÞ � sð0:5kiÞ1:5sðkiÞ (1)
where s is ignition delay and ki is species rate coefficient.
Negative value of sensitivity coefficient indicates a promotion
effect on the total reaction rate while positive value of sensi-
tivity coefficient indicates an inhibition effect on the total
reaction rate.
4.2.1. Reaction system in MCDI mixturesThe sensitivity analysis of the 80%CH4/20%H2 mixture was
made, as shown in Fig. 8. At T ¼ 1400 K, the main ignition
promotion reactions R1, R93 and R96 are identified. Moreover,
the key ignition inhibition reactions are the chain termination
reaction R104 and the consumption reactions of methane
R123, R124 and R125. The sensitivity coefficients of ignition
promotion reactions R1 decreases with increase in equiva-
lence ratio, thus the chain branching efficiency is inhibited
through reaction R1, and decreases the accelerated rate of
total reaction. The sensitivity coefficients of reactions R124
and R125 decrease with increase in equivalence ratio, thus the
inhibition effect on rate of total reaction is weakened.
Furthermore, the reactions R93 and R96 which are the reac-
tions in production of CH3O radical become importantly at
high temperature and promote the ignition since CH3 radical
is consumed and free radicals O and OH are produced through
Fig. 7 e Measured and calculated ignition delays for
hydrogen using different kinetic models. (a) f [ 0.5, (b)
f [ 1.0, (c) f [ 2.0.
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716717718719720721722723724725726727728729730731732733734735736737738739740741742743744745746747748749750751752753754755756757758759760761762763764765766767768769770771772773774775776777778779780
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R93 and R96 respectively. The sensitivity coefficients of R93
and R96 decreasewith increase in equivalence ratio, leading to
the weakening on accelerated ignition tendency. It is note-
worthy that both reactions R104 which is recombination
reaction of two CH3 radicals and R123 which is H-scavenging
reaction are insensitive to the variation of equivalence ratio.
Thus, overall the ignition of the mixtures is inhibited with
increase in equivalence ratio and this is consistent to the
experimental results in Fig. 3(b).
At T¼ 930 K, the chemistries of HO2 and H2O2 becomemore
important such as reactions R14, R19, R22, R86, R95 and R96. It
is clearly identified that R96 plays the most important ignition
promotion reaction instead of R1. The sensitivity coefficient of
R96 decreases with increase in equivalence ratio, and the
ignition promotion effect is weakened. Furthermore, the
sensitivity coefficient of R104 increases and that of R86 and
R94 decrease with increase in equivalence ratio, as the result
the ignition inhibition effect is promoted. Therefore, for low
temperature, the ignition is inhibited and ignition delay is
increased with increase in equivalence ratio.
4.2.2. Reaction system in CCMHDI mixtureFig. 9 gives the sensitivity analysis of the 60%CH4/40%H2
mixture. At T ¼ 1400 K, the result indicates that almost all of
the key elementary reactions are frommethane chemistry for
this mixture. Therefore, the dependence of ignition delay on
equivalence ratio is similar to the reaction system inmethane
chemistry dominating ignition, and related analysis and
discussion are not included in this part.
At T ¼ 930 K, however, the hydrogen chemistry becomes
also very important except the methane chemistry. The
sensitivity coefficient of the reaction R14 increases with
increase in equivalence ratio, and the H2O2 radical produced
by R14 will provide the contributions toward two different
aspects. One is that the rates of ignition promotion reactions
R97 and R25 are promoted and the sensitivity coefficient
increases with increase in equivalence ratio. Thus the ignition
promotion effect is enhanced. The other is that the rate of
ignition inhibition reaction R19 is also promoted by HO2
radical produced through R25 and the sensitivity coefficient
Fig. 8 e Normalized sensitivity analysis of ignition delays
for the 80%CH4/20%H2 mixture using USC Mech 2.0. (a)
T [ 1400 K, (b) T [ 930 K.
Fig. 9 e Normalized sensitivity analysis of ignition delays
for 40%CH4/60%H2 mixture using USC Mech 2.0. (a)
T [ 1400 K, (b) T [ 930 K.
i n t e rn a t i o n a l j o u rn a l o f h y d r o g e n en e r g y x x x ( 2 0 1 2 ) 1e9 7
781782783784785786787788789790791792793794795796797798799800801802803804805806807808809810811812813814815816817818819820821822823824825826827828829830831832833834835836837838839840841842843844845
846847848849850851852853854855856857858859860861862863864865866867868869870871872873874875876877878879880881882883884885886887888889890891892893894895896897898899900901902903904905906907908909910
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increases with increase in equivalence ratio. Thus the ignition
promotion effect is weakened. Furthermore, it is identified
that the reaction R96 competes the CH3 radical to that of R97,
and these two reactions result in an opposite influence on
ignition delay with variation of equivalence ratio. Thus, the
ignition delay is insensitive to equivalence ratio at low
temperature region for the 60%CH4/40%H2 mixture, and this is
consistent to the experimental results in Fig. 4.
4.2.3. Reaction system in HCDI mixturesThe sensitivity analysis of the 20%CH4/80%H2 mixture was
made to study the effects of equivalence ratio on ignition
delay, as shown in Fig. 10. At T ¼ 1400 K, the reactions R2 and
R3 become more important in addition to reaction R1. The
sensitivity coefficients of the reactions R2 and R3 decrease
with increase in equivalence ratio, and the ignition promotion
is weakened. Moreover, the sensitivity coefficient of H-scav-
enging reaction R88 increases with increase in equivalence
ratio. Thus the rate of total reaction is decreased and ignition
delay is increased. It is noteworthy that the maximum values
of sensitivity coefficients of competition reactions R1 and R123
occur at f ¼ 1.0, which suggests the strongest inhibition effect
on ignition at the stoichiometric equivalence ratio. It is
because of these complex dependencies of the key elementary
reactions to equivalence ratio, a complex effect of equivalence
ratio on ignition delays is demonstrated in Fig. 5(a).
At T¼ 930 K, the chemistries of HO2 and H2O2 dominate the
ignition of fuel mixture. The chain termination reactions R18,
R19 and R22 become key ignition inhibition reactions instead
of the consumption reactions of methane R123, R124 and
R125. Analysis indicates that the sensitivity coefficients of
reactions R14 and R25 increase with increase in equivalence
ratio, thus the ignition promotion effect is enhanced through
these two reactions. However, the sensitivity coefficient of
reaction R1 decreases with increase in equivalence ratio,
which weakens the ignition promotion effect. It is identified
that R1 is main competitor to R25 for H radical. If reaction R1
dominates the ignition chemistry, the ignition delays will
increase with increase in equivalence ratio, and this case is
more likely appearing under the leanmixture condition due to
sufficient oxygen molecular. However, if the reaction R25
dominates the ignition chemistry, the ignition delays will
decrease with increase in equivalence ratio and this case is
more likely appearing under the richmixture condition. Thus,
the insensitive effect of equivalence ratio on ignition as
shown in Fig. 5(a) may be attributed to the competition
between R1 and R25. Furthermore, the sensitivity coefficient
of the ignition promotion reaction R97 increases with
increasing the equivalence ratio.
It is noted that the ignition characteristics of HCDI
mixtures at middle-low temperature are similar to those of
CCMHDI mixtures, although ignition mechanisms are
different as discussed by above.
5. Conclusions
Experimental and modeling studies on ignition delays of the
methane/hydrogen mixtures with various hydrogen volu-
metric contents (0%, 20%, 40%, 60%, 80% and 100%) were
conducted at engine relevant pressure using a shock tube.
Main conclusions are summarized as follows:
1. For MCDI mixtures ðXH2 � 40%Þ, at high temperature, the
ignition promotion is weakened with increasing equiva-
lence ratio by reaction R1 because ignition kinetic mainly
depends on oxygen concentration. At middle-low temper-
ature, the ignition inhibition is enhanced with increasing
equivalence ratio by the chemistries of CH3 and HO2
because ignition kinetic more depends on fuel concentra-
tion. Therefore, increasing equivalence ratio reduces the
ignition delay in this study. The non-linear relationship
between logarithmic of ignition delay and equivalence ratio
becomes increasingly apparent with increasing hydrogen
fraction.
2. For CCMHDI mixture ðXH2 ¼ 60%Þ, at high temperature, the
dependence of ignition delay on equivalence ratio is similar
to that of methane chemistry dominating reaction system.
At middle-low temperature, the ignition delays are insen-
sitive to the variation of equivalence ratio.When increasing
Fig. 10 e Normalized sensitivity analysis of ignition delays
for 20%CH4/80%H2 mixture using USC Mech 2.0. (a)
T [ 1400 K, (b) T [ 930 K.
i n t e r n a t i o n a l j o u r n a l o f h y d r o g e n en e r g y x x x ( 2 0 1 2 ) 1e98
911912913914915916917918919920921922923924925926927928929930931932933934935936937938939940941942943944945946947948949950951952953954955956957958959960961962963964965966967968969970971972973974975
976977978979980981982983984985986987988989990991992993994995996997998999
10001001100210031004100510061007100810091010101110121013101410151016101710181019102010211022102310241025102610271028102910301031103210331034103510361037103810391040
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the equivalence ratio, the H2O2 produced through reaction
R14 promotes the rates of ignition promotion reaction R97
and ignition inhibition reaction R19, and this leads to
balanced influence of equivalence ratio on ignition delay.
3. For HCDI mixtures ðXH2 � 80%Þ, ignition delays give
a complex dependence on equivalence ratio. At high
temperature, the maximum values of the sensitivity coef-
ficient of the key elementary reactions appear at stoichio-
metric ratio, and this leads to the shortest ignition delay at
f ¼ 1.0. At middle-low temperature, the hydrogen chem-
istry becomes more obvious, and the effect of equivalence
ratio on ignition delay ismainly due to contribution of the H
competition reactions (R1 and R25) and CH3 competition
reactions (R96 and R97) on ignition kinetic.
Acknowledgments
This work is supported by the National Natural Science
Foundation of China (Grant No. 51136005, 51121092).
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