1997
DOI: 10.1002/(sici)1097-4601(1997)29:7<483::aid-kin2>3.0.co;2-q
|View full text |Cite
|
Sign up to set email alerts
|

A shock tube study of the pyrolysis of NO2

Abstract: NO 2 concentration profiles in shock-heated NO 2 /Ar mixtures were measured in the temperature range of 1350 -2100 K and pressures up to 380 atm using Ar ϩ laser absorption at 472.7 nm, IR emission at , and visible emission at 300 -600 nm. In the course of this study, the absorption coefficient of NO 2 at 472.7 nm was measured at temperatures from 300 K to 2100 K and pressures up to 75 atm. Rate coefficients for the reactions and were derived by comparing the measured and calculated NO 2 profiles. For reaction… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

5
17
0

Year Published

2000
2000
2016
2016

Publication Types

Select...
4
2
1

Relationship

1
6

Authors

Journals

citations
Cited by 27 publications
(24 citation statements)
references
References 27 publications
5
17
0
Order By: Relevance
“…At 2700 K, the computed rate coefficient compares favourably with experimental data. 53,54 No correction was made for zero-point energy (ZPE) and other quantum effects, such as tunneling through the centrifugal barrier which can be still significant at low temperatures. The centrifugal barrier originates from the conservation of the total angular momentum and consists of the rotational energy associated with the orbital angular momentum of the colliding partner with respect to the center of mass of the whole system.…”
Section: B Thermal Rate Coefficientsmentioning
confidence: 99%
“…At 2700 K, the computed rate coefficient compares favourably with experimental data. 53,54 No correction was made for zero-point energy (ZPE) and other quantum effects, such as tunneling through the centrifugal barrier which can be still significant at low temperatures. The centrifugal barrier originates from the conservation of the total angular momentum and consists of the rotational energy associated with the orbital angular momentum of the colliding partner with respect to the center of mass of the whole system.…”
Section: B Thermal Rate Coefficientsmentioning
confidence: 99%
“…The recombination reaction between NO and O to form NO 2 (R31) is well‐characterized across wide temperature and pressure intervals, i.e. 117–120, and old 121 and recent 41 reviews are generally in good agreement. The present mechanism uses high‐ and low‐pressure limits from Tsang and Herron including falloff parameters.…”
Section: Detailed Kinetic Modelmentioning
confidence: 88%
“…through NO+NO+O 2 ⇋ NO 2 +NO 2 ⇋ N 2 O 4 , whereas increasing temperatures promote the reverse decomposition reactions. A shock tube study of the thermal decay of NO 2 by Röhrig et al 119 has recently provided experimental data for (R42) and (R43) at high temperatures (1350–2100 K). Park et al 145 combined these data for (R42) with pyrolysis measurements for NO x at intermediate temperatures (602–954 K) to obtain an expression of k 42 across the temperature range 600–1450 K. Data of (–R42) are also available at intermediate temperatures: Olbregts 147 conducted static reactor experiments with NO/O 2 mixtures at temperatures from 226 to 758 K to yield an expression of k −42 that agrees within 15% of the expression of Park et al at temperatures from 600 to 1450 K, when using thermodynamic data from Table I to calculate k 42 .…”
Section: Detailed Kinetic Modelmentioning
confidence: 99%
“…Unfortunately, when performing chemistry measurements in a shock tube, errors in the reaction temperature can lead to large uncertainties in the rate coefficient or ignition delay time [1]. For example, the high-pressure rate coefficient of N0 2 has an activation energy of 300 kJ/mol (i.e., k^T) = 4xl0 14 exp(300/RT) ) [2]. For an average temperature of 1500 K, a 15-K error in temperature (i.e., only 1%) can lead to a 25% uncertainty in the measured rate coefficient.…”
Section: Introductionmentioning
confidence: 99%