6096 J. Phys. Chem. A, Vol. 106, No. 25, 2002
Song et al.
TABLE 2: Inputs for the RRKM Calculations
average energy transferred in a single collision, 〈∆E〉all. Since
the 〈∆E〉all value depends mostly on the bath gas (argon) rather
than the reactant (benzylamine) and is a very weak function of
T, we can estimate the range of 〈∆E〉all values of benzylamine-
argon collisions even though experimental data are not available.
C6H5CH2NH2 (Molecule)
frequencies (cm-1)
3405, 3335, 3060, 3050, 3040, 3025,
3
1
1
1
8
3
025, 2945, 2910, 1600, 1580, 1560,
465, 1430, 1425, 1335, 1315, 1300,
280, 1170, 1155, 1135, 1110, 1050,
035, 1010, 975, 960, 935, 890, 875, 850,
20, 770, 735, 685, 610, 565, 475, 395,
-
1
The estimated 〈∆E〉all was -150 ( 50 cm , which is similar
1
5
to that in toluene-argon collisions. After determining the
〈∆E〉all value and calculating âc from a given 〈∆E〉all, we obtained
E0 within uncertainty limits corresponding to the range of A∞
values.
50, 310, 245, 130, 45
5
product of adiabatic moments 4.022 × 10
-
80
2
4
of inertia (10 g cm )
Moment of inertia for active
182.2
-
40
2
external rotor (10 g cm )
To reduce the uncertainty of the E0 values, we needed to use
(1) more accurate values of A∞ or (2) other independent
experimental data. To obtain the true value of A∞, experiments
should be performed at sufficiently high pressure. However,
Brouwer and co-workers have reported that the ethylbenzene
decomposition reaction (R2) was still in the falloff regime even
C6H5CH2‚‚‚NH2 (Transition State)
3305, 3230, 3115, 3065, 3055, 3050,
frequencies (cm-1)
3
1
1
9
4
040, 3035, 3025, 1530, 1515, 1495,
445, 1440, 1420, 1305, 1270, 1235,
140, 1130, 1075, 995, 960, 955, 940,
35, 865, 800, 745, 680, 660, 605, 515,
85, 460, 375, 345,190
13
at the highest experimental pressure, which was 20 times
5
product of adiabatic moments 9.097 × 10 at 1150 K
-
80
2
4
5
higher than our experimental pressure. So instead, we reanalyzed
the VLPP experimental data to obtain values of E0 and A∞ more
accurately.
of inertia (10 g cm )
8.696 × 10 at 1400 K
moment of inertia for active
253.5
-
40
2
external rotor (10 g cm )
moment of inertia for active
2.012 (σ ) 2), 376.8 (σ ) 1)
2.145 (σ ) 3)
-
40
2
In contrast to the shock tube data analysis, where energy
transfer is with gas-gas collisions, the efficiency of a gas-
wall collision used in the VLPP, âw, was required for the RRKM
calculations. For some molecules, the âw values were obtained
experimentally, but data for benzylamine were not available,
so we estimated the range of âw values on the basis of a study
2
-D rotor (10 g cm )
moment of inertia for active
-
40
2
1
-D rotor (10 g cm )
TABLE 3: Data Used in Eq 4
species
T (K)
∆
f
H° (kJ mol-1)
uncertainty
ref
benzylamine
0
0
115.5
192
(2.7
(1
23
24
16
by Dick et al., who pointed out that gas-wall collision under
NH
2
VLPP conditions had collision efficiencies of âw ) 0.5 ( 0.1.
4
16
In the VLPP study performed prior to the work of Dick et al.,
the percentage of the 4π steradians unavailable to the rotating
species. In effect, we are treating the rotations by varying the
rotational level spacing through use of η, thereby controlling
the entropy and heat capacity of the transition state. The
hindrance is introduced into the RRKM code by multiplying
the adiabatic two-dimensional rotor moments of inertia of the
NH2 and benzyl fragments in the transition state each by (1 -
a unit gas-wall collision efficiency (âw ) 1) was used. From
the RRKM calculations with the given input parameters, we
obtained combinations of A∞ and E0 fitting the VLPP as well
as the shock tube data. The ranges of the 〈∆E〉all and âw values
automatically determine the uncertainty of the A∞ and E0 values.
In addition to the RRKM calculations, we used the Multiwell
1
7,18
code,
which solves the master equation using a stochastic
1
/2
η) .
To analyze the shock tube data alone, employing the RRKM
method. The average energy transfer used for deactivating
-
1
collisions with argon, 〈∆E〉down, was 550 cm corresponding
calculations, we had to estimate the high-pressure A factor, A∞.
The input parameters for the RRKM calculations cannot be
determined by a single set of experimental data; therefore, either
E0 or A∞ has to be estimated reasonably. We assumed that
ethylbenzene (C6H5CH2CH3) decomposition chemistry was
similar to that of benzylamine decomposition and used the A∞
values of ethylbenzene for the RRKM calculations of benzyl-
amine decomposition.
-
1
to 〈∆E〉all ) -150 cm , and the results of the Multiwell
calculation were consistent with those of the RRKM calcula-
1
9
tions.
The frequencies and moments of inertia of the molecule and
transition state were calculated using Gaussian 98, revision 7,20
at the B3LYP/6-311G(d,p) level, and are tabulated in Table 3
with other input parameters for the RRKM calculation.
C H CH CH f CH + C H CH
(R2)
Results and Discussion
6
5
2
3
3
6
5
2
From the RRKM calculations, we determined the high-
pressure-limit rate, k∞, and the bond dissociation energy of
the C-N bond of benzylamine at 0 K. Using the input
parameters given in Table 3, the high-pressure rates were
calculated every 100 K from 1000 to 1600 K. Fitting these rate
coefficients linearly on an Arrhenius plot, we derived the rate
expression
1
1
According to Baulch et al.’s review, the recommended A∞
15 -1
value for reaction R2 is 7.1 × 10
s
for the temperature range
70-1800 K. Considering only papers published since 1980,
7
1
2
13
15
the minimum and maximum values were 2.0 × 10 and
1
7 -1
1
.3 × 10 s , respectively. We set the uncertainty of A∞ as a
factor of 4, and the corresponding range of A∞ used for the
15
16 -1
RRKM calculations was from 1.6 × 10 to 2.5 × 10 s .
Within this range of A∞, we calculated η and found the
relationship between A∞ and η at the mean temperature of the
experimental conditions.
-
1
16
k /s ) 1.07 × 10 exp[-36470/[T (K)]] (1000 K < T <
∞
1600 K) (2)
As stated earlier, RRKM calculations also require some
knowledge of energy transfer. The simple pseudo-strong-
collision version seems adequate for this study, which means
knowing the value of the collision efficiency, âc. Troe has
suggested that the collision efficiency, âc, is related to the
The A∞ value given in eq 2 is 7 times the A∞ value reported by
Golden et al. and 50% higher than the A factor for the
4
1
4
ethylbenzene decomposition reaction recommended by Baulch
1
1
et al. The lower temperature limit of our experiments corre-