Tom Bowman
Professor of Mechanical Engineering, Emeritus
Bio
Professor Bowman studies reacting flows, primarily through experimental means, and the processes by which pollutants are formed and destroyed in flames. In addition, he is interested in the environmental impact of energy use, specifically greenhouse gas emissions from use of fossil fuels.
Academic Appointments
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Emeritus Faculty, Acad Council, Mechanical Engineering
Honors & Awards
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Research Prize, Humboldt (1997)
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Zeldovich Gold Medal, Combustion Institute (1998)
Boards, Advisory Committees, Professional Organizations
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Member, National Academy of Engineering (2013 - Present)
Professional Education
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PhD, Princeton, Aerospace and Mechanical Sciences (1966)
2022-23 Courses
- Combustion Fundamentals
ME 371 (Win) -
Independent Studies (8)
- Engineering Problems
ME 391 (Aut, Win, Spr, Sum) - Engineering Problems and Experimental Investigation
ME 191 (Aut, Win, Spr, Sum) - Experimental Investigation of Engineering Problems
ME 392 (Aut, Win, Spr, Sum) - Honors Research
ME 191H (Aut, Win, Spr, Sum) - Ph.D. Research Rotation
ME 398 (Aut, Win, Spr) - Practical Training
ME 199A (Aut) - Practical Training
ME 299A (Aut, Win, Spr, Sum) - Practical Training
ME 299B (Aut, Win, Spr, Sum)
- Engineering Problems
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Prior Year Courses
2021-22 Courses
- Combustion Applications
ME 372 (Spr) - Combustion Fundamentals
ME 371 (Win) - Physical Gas Dynamics
ME 362A (Aut)
- Combustion Applications
All Publications
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Professor Irvin Glassman
COMBUSTION SCIENCE AND TECHNOLOGY
2021; 193 (4): 539–40
View details for DOI 10.1080/00102202.2020.1841180
View details for Web of Science ID 000614806000001
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Impact of vitiation on flow reactor studies of jet fuel combustion chemistry
COMBUSTION AND FLAME
2021; 224: 66–72
View details for DOI 10.1016/j.combustflame.2020.10.044
View details for Web of Science ID 000609127800009
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Professor Irvin Glassman (1923-2019) IN MEMORIAM
COMBUSTION AND FLAME
2021; 223: A1
View details for DOI 10.1016/j.combustflame.2020.10.027
View details for Web of Science ID 000599642700001
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A physics-based approach to modeling real-fuel combustion chemistry - V. NOx formation from a typical Jet A
COMBUSTION AND FLAME
2020; 212: 270–78
View details for DOI 10.1016/j.combustflame.2019.10.038
View details for Web of Science ID 000515192500023
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Kinetic analysis of distinct product generation in oxidative pyrolysis of four octane isomers
PROCEEDINGS OF THE COMBUSTION INSTITUTE
2019; 37 (1): 531–38
View details for DOI 10.1016/j.proci.2018.06.219
View details for Web of Science ID 000456612200051
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A Physics-based approach to modeling real-fuel combustion chemistry - III. Reaction kinetic model of JP10
COMBUSTION AND FLAME
2018; 198: 466–76
View details for DOI 10.1016/j.combustflame.2018.08.022
View details for Web of Science ID 000452581400039
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A physics based approach to modeling real-fuel combustion chemistry - IV. HyChem modeling of combustion kinetics of a bio-derived jet fuel and its blends with a conventional Jet A
COMBUSTION AND FLAME
2018; 198: 477–89
View details for DOI 10.1016/j.combustflame.2018.07.012
View details for Web of Science ID 000452581400040
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A physics-based approach to modeling real-fuel combustion chemistry - II. Reaction kinetic models of jet and rocket fuels
COMBUSTION AND FLAME
2018; 193: 520–37
View details for DOI 10.1016/j.combustflame.2018.03.021
View details for Web of Science ID 000436899700042
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A physics-based approach to modeling real-fuel combustion chemistry - I. Evidence from experiments, and thermodynamic, chemical kinetic and statistical considerations
COMBUSTION AND FLAME
2018; 193: 502–19
View details for DOI 10.1016/j.combustflame.2018.03.019
View details for Web of Science ID 000436899700041
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An experimental and kinetic modeling study of n-dodecane pyrolysis and oxidation
COMBUSTION AND FLAME
2016; 163: 12-30
View details for DOI 10.1016/j.combustflame.2015.08.005
View details for Web of Science ID 000367278600002
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Shock Tube Measurements of the Rate Constant for the Reaction Ethanol + OH.
journal of physical chemistry. A
2014; 118 (5): 822-828
Abstract
The overall rate constant for the reaction ethanol + OH → products was determined experimentally from 900 to 1270 K behind reflected shock waves. Ethan(18)ol was utilized for these measurements in order to avoid the recycling of OH radicals following H-atom abstraction at the β-site of ethanol. Similar experiments were also performed with unlabeled ethan(16)ol in order to infer the rate constant that excludes reactivity at the β-site. The two data sets were used to directly infer the branching ratio for the reaction at the β-site. Experimental data in the current study and in previous low-temperature studies for the overall rate constant are best fit by the expression koverall = 5.07 × 10(5) T[K](2.31) exp(608/T[K]) cm(3) mol(-1) s(-1), valid from 300 to 1300 K. Measurements indicate that the branching ratio of the β-site is between 20 and 25% at the conditions studied. Pseudo-first-order reaction conditions were generated using tert-butylhydroperoxide (TBHP) as a fast source of (16)OH with ethanol in excess. (16)OH mole fraction time-histories were measured using narrow-line width laser absorption near 307 nm. Measurements were performed at the linecenter of the R22(5.5) transition in the A-X(0,0) band of (16)OH that does not overlap with any absorption features of (18)OH, thus producing a measurement of the (16)OH mole fraction that is insensitive to the presence of (18)OH.
View details for DOI 10.1021/jp410853f
View details for PubMedID 24405356
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Shock Tube Measurements of the Rate Constant for the Reaction Ethanol plus OH
JOURNAL OF PHYSICAL CHEMISTRY A
2014; 118 (5): 822-828
Abstract
The overall rate constant for the reaction ethanol + OH → products was determined experimentally from 900 to 1270 K behind reflected shock waves. Ethan(18)ol was utilized for these measurements in order to avoid the recycling of OH radicals following H-atom abstraction at the β-site of ethanol. Similar experiments were also performed with unlabeled ethan(16)ol in order to infer the rate constant that excludes reactivity at the β-site. The two data sets were used to directly infer the branching ratio for the reaction at the β-site. Experimental data in the current study and in previous low-temperature studies for the overall rate constant are best fit by the expression koverall = 5.07 × 10(5) T[K](2.31) exp(608/T[K]) cm(3) mol(-1) s(-1), valid from 300 to 1300 K. Measurements indicate that the branching ratio of the β-site is between 20 and 25% at the conditions studied. Pseudo-first-order reaction conditions were generated using tert-butylhydroperoxide (TBHP) as a fast source of (16)OH with ethanol in excess. (16)OH mole fraction time-histories were measured using narrow-line width laser absorption near 307 nm. Measurements were performed at the linecenter of the R22(5.5) transition in the A-X(0,0) band of (16)OH that does not overlap with any absorption features of (18)OH, thus producing a measurement of the (16)OH mole fraction that is insensitive to the presence of (18)OH.
View details for DOI 10.1021/jp410853f
View details for Web of Science ID 000331153400004
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Shock Tube Measurements of the tert-Butanol + OH Reaction Rate and the tert-C4H8OH Radical ß-Scission Branching Ratio Using Isotopic Labeling.
journal of physical chemistry. A
2013; 117 (23): 4777-4784
Abstract
The overall rate constant for the reaction tert-butanol + OH → products was determined experimentally behind reflected shock waves by using (18)O-substituted tert-butanol (tert-butan(18)ol) and tert-butyl hydroperoxide (TBHP) as a fast source of (16)OH. The data were acquired from 900 to 1200 K near 1.1 atm and are best fit by the Arrhenius expression 1.24 × 10(-10) exp(-2501/T [K]) cm(3) molecule(-1) s(-1). The products of the title reaction include the tert-C4H8OH radical that is known to have two major β-scission decomposition channels, one of which produces OH radicals. Experiments with the isotopically labeled tert-butan(18)ol also lead to an experimental determination of the branching ratio for the β-scission pathways of the tert-C4H8OH radical by comparing the measured pseudo-first-order decay rate of (16)OH in the presence of excess tert-butan(16)ol with the respective decay rate of (16)OH in the presence of excess tert-butan(18)ol. The two decay rates of (16)OH as a result of reactions with the two forms of tert-butanol differ by approximately a factor of 5 due to the absence of (16)OH-producing pathways in experiments with tert-butan(18)ol. This indicates that 80% of the (16)OH molecules that react with tert-butan(16)ol will reproduce another (16)OH molecule through β-scission of the resulting tert-C4H8(16)OH radical. (16)OH mole fraction time histories were measured using narrow-line-width laser absorption near 307 nm. Measurements were performed at the line center of the R22(5.5) transition in the A-X(0,0) band of (16)OH, a transition that does not overlap with any absorption features of (18)OH, hence yielding a measurement of (16)OH mole fraction that is insensitive to any production of (18)OH.
View details for DOI 10.1021/jp402176e
View details for PubMedID 23683356
- CFD simulation of a confined axisymmetric laminar methane-air diffusion flame 8th Mediterranean Combustion Symposium 2013
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Experimental Determination of the High-Temperature Rate Constant for the Reaction of OH with sec-Butanol
JOURNAL OF PHYSICAL CHEMISTRY A
2012; 116 (39): 9607-9613
Abstract
The overall rate constant for the reaction of OH with sec-butanol [CH(3)CH(OH)CH(2)CH(3)] was determined from measurements of the near-first-order OH decay in shock-heated mixtures of tert-butylhydroperoxide (as a fast source of OH) with sec-butanol in excess. Three kinetic mechanisms from the literature describing sec-butanol combustion were used to examine the sensitivity of the rate constant determination to secondary kinetics. The overall rate constant determined can be described by the Arrhenius expression 6.97 × 10(-11) exp(-1550/T[K]) cm(3) molecule(-1) s(-1), valid over the temperature range of 888-1178 K. Uncertainty bounds of ±30% were found to adequately account for the uncertainty in secondary kinetics. To our knowledge, the current data represent the first efforts toward an experimentally determined rate constant for the overall reaction of OH with sec-butanol at combustion-relevant temperatures. A rate constant predicted using a structure-activity relationship from the literature was compared to the current data and previous rate constant measurements for the title reaction at atmospheric-relevant temperatures. The structure-activity relationship was found to be unable to correctly predict the measured rate constant at all temperatures where experimental data exist. We found that the three-parameter fit of 4.95 × 10(-20)T(2.66) exp(+1123/T[K]) cm(3) molecule(-1) s(-1) better describes the overall rate constant for the reaction of OH with sec-butanol from 263 to 1178 K.
View details for DOI 10.1021/jp306977e
View details for Web of Science ID 000309375300002
View details for PubMedID 22946741
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High-Temperature Rate Constant Determination for the Reaction of OH with iso-Butanol
JOURNAL OF PHYSICAL CHEMISTRY A
2012; 116 (19): 4720-4725
Abstract
This work presents the first direct experimental study of the rate constant for the reaction of OH with iso-butanol (2-methyl-1-propanol) at temperatures from 907 to 1147 K at near-atmospheric pressures. OH time-histories were measured behind reflected shock waves using a narrow-linewidth laser absorption method during reactions of dilute mixtures of tert-butylhydroperoxide (as a fast source of OH) with iso-butanol in excess. The title reaction's overall rate constant (OH + iso-butanol →(k(overall)) all products) minus the rate constant for the β-radical-producing channel (OH + iso-butanol →(k(β)) 1-hydroxy-2-methyl-prop-2-yl radical + H(2)O) was determined from the pseudo-first-order rate of OH decay. A two-parameter Arrhenius fit of the experimentally determined rate constant in the current temperature range yields the expression (k(overall) - k(β)) = 1.84 × 10(-10) exp(-2350/T[K]) cm(3) molecule(-1) s(-1). A recommendation for the overall rate constant, including k(β), is made, and comparisons of the results to rate constant recommendations from the literature are discussed.
View details for DOI 10.1021/jp302719j
View details for Web of Science ID 000304073200005
View details for PubMedID 22515280
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Rate Constant Measurements for the Overall Reaction of OH+1-Butanol -> Products from 900 to 1200 K
JOURNAL OF PHYSICAL CHEMISTRY A
2012; 116 (10): 2475-2483
Abstract
The rate constant for the overall reaction OH + 1-butanol → products was determined in the temperature range 900 to 1200 K from measurements of OH concentration time histories in reflected shock wave experiments of tert-butyl hydroperoxide (TBHP) as a fast source of OH radicals with 1-butanol in excess. Narrow-linewidth laser absorption was employed for the quantitative OH concentration measurement. A detailed kinetic mechanism was constructed that includes updated rate constants for 1-butanol and TBHP kinetics that influence the near-first-order OH concentration decay under the present experimental conditions, and this mechanism was used to facilitate the rate constant determination. The current work improves upon previous experimental studies of the title rate constant by utilizing a rigorously generated kinetic model to describe secondary reactions. Additionally, the current work extends the temperature range of experimental data in the literature for the title reaction under combustion-relevant conditions, presenting the first measurements from 900 to 1000 K. Over the entire temperature range studied, the overall rate constant can be expressed in Arrhenius form as 3.24 × 10(-10) exp(-2505/T [K]) cm(3) molecule(-1) s(-1). The influence of secondary reactions on the overall OH decay rate is discussed, and a detailed uncertainty analysis is performed yielding an overall uncertainty in the measured rate constant of ±20% at 1197 K and ±23% at 925 K. The results are compared with previous experimental and theoretical studies on the rate constant for the title reaction and reasonable agreement is found when the earlier experimental data were reinterpreted.
View details for DOI 10.1021/jp211885p
View details for Web of Science ID 000301509400010
View details for PubMedID 22352920
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High-Temperature Measurements of the Rate Constants for Reactions of OH with a Series of Large Normal Alkanes: n-Pentane, n-Heptane, and n-Nonane
ZEITSCHRIFT FUR PHYSIKALISCHE CHEMIE-INTERNATIONAL JOURNAL OF RESEARCH IN PHYSICAL CHEMISTRY & CHEMICAL PHYSICS
2011; 225 (11-12): 1157-1178
View details for DOI 10.1524/zpch.2011.0156
View details for Web of Science ID 000299393700002
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Vitiated ethane oxidation in a high-pressure flow reactor
COMBUSTION AND FLAME
2009; 156 (10): 1886-1897
View details for DOI 10.1016/j.combustflame.2009.05.012
View details for Web of Science ID 000274583500004
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High-temperature shock tube study of the reactions CH3+OH -> products and CH3OH+Ar -> products
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
2008; 40 (8): 488-495
View details for DOI 10.1002/kin.20334
View details for Web of Science ID 000257769400004
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Shock tube study of the reaction of CH with N-2: Overall rate and branching ratio
JOURNAL OF PHYSICAL CHEMISTRY A
2007; 111 (46): 11818-11830
Abstract
We have studied the reaction between CH and N2, (1) CH + N2 --> products, in shock tube experiments using CH and NCN laser absorption. CH was monitored by continuous-wave, narrow-line-width laser absorption at 431.1 nm. The overall rate coefficient of the CH + N2 reaction was measured between 1943 and 3543 K, in the 0.9-1.4 atm pressure range, using a CH perturbation approach. CH profiles recorded upon shock-heating dilute mixtures of ethane in argon and acetic anhydride in argon were perturbed by the addition of nitrogen. The perturbation in the CH concentration was principally due to the reaction between CH and N2. Rate coefficients for the overall reaction were inferred by kinetically modeling the perturbed CH profiles. A least-squares, two-parameter fit of the current overall rate coefficient measurements was k1 = 6.03 x 1012 exp(-11150/T [K]) (cm3 mol-1 s-1). The uncertainty in k1 was estimated to be approximately +/-25% and approximately +/-35% at approximately 3350 and approximately 2100 K, respectively. At high temperatures, there are two possible product channels for the reaction between CH and N2, (1a) CH + N2 --> HCN + N and (1b) CH + N2 --> H + NCN. The large difference in the rates of the reverse reactions enabled inference of the branching ratio of reaction 1, k1b/(k1b + k1a), in the 2228-2905 K temperature range by CH laser absorption in experiments in a nitrogen bath. The current CH measurements are consistent with a branching ratio of 1 and establish NCN and H as the primary products of the CH + N2 reaction. A detailed and systematic uncertainty analysis, taking into account experimental and mechanism-induced contributions, yields a conservative lower bound of 0.70 for the branching ratio. NCN was also detected by continuous-wave, narrow-line-width laser absorption at 329.13 nm. The measured NCN time histories were used to infer the rate coefficient of the reaction between H and NCN, H + NCN --> HCN + N, and to estimate an absorption coefficient for the NCN radical.
View details for DOI 10.1021/jp075638c
View details for Web of Science ID 000250967800012
View details for PubMedID 17958405
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Effects of pressure on performance of mesoscale burner arrays for gas-turbine applications
JOURNAL OF PROPULSION AND POWER
2007; 23 (4): 884-886
View details for DOI 10.2514/1.26255
View details for Web of Science ID 000248073000032
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High-temperature shock tube measurements of methyl radical decomposition
JOURNAL OF PHYSICAL CHEMISTRY A
2007; 111 (19): 4062-4072
Abstract
We have studied the two-channel thermal decomposition of methyl radicals in argon, involving the reactions CH3 + Ar --> CH + H2 + Ar (1a) and CH3 + Ar --> CH2 + H + Ar (1b), in shock tube experiments over the 2253-3527 K temperature range, at pressures between 0.7 and 4.2 atm. CH was monitored by continuous-wave, narrow-line-width laser absorption at 431.1311 nm. The collision-broadening coefficient for CH in argon, 2gamma(CH-Ar), was measured via repeated single-frequency experiments in the ethane pyrolysis system behind reflected shock waves. The measured 2gamma(CH-Ar) value and updated spectroscopic and molecular parameters were used to calculate the CH absorption coefficient at 431.1311 nm (23194.80 cm(-1)), which was then used to convert raw traces of fractional transmission to quantitative CH concentration time histories in the methyl decomposition experiments. The rate coefficient of reaction 1a was measured by monitoring CH radicals generated upon shock-heating highly dilute mixtures of ethane, C2H6, or methyl iodide, CH3I, in an argon bath. A detailed chemical kinetic mechanism was used to model the measured CH time histories. Within experimental uncertainty and scatter, no pressure dependence could be discerned in the rate coefficient of reaction 1a in the 0.7-4.2 atm pressure range. A least-squares, two-parameter fit of the current measurements, applicable between 2706 and 3527 K, gives k(1a) (cm(3) mol(-1) s(-1)) = 3.09 x 1015 exp[-40700/T (K)]. The rate coefficient of reaction 1b was determined by shock-heating dilute mixtures of C2H6 or CH3I and excess O2 in argon. During the course of reaction, OH radicals were monitored using the well-characterized R(1)(5) line of the OH A-X (0,0) band at 306.6871 nm (32606.52 cm(-1)). H atoms generated via reaction 1b rapidly react with O2, which is present in excess, forming OH. The OH traces are primarily sensitive to reaction 1b, reaction 9 (H + O2 --> OH + O) and reaction 10 (CH3 + O2 --> products), where the rate coefficients of reactions 9 and 10 are relatively well-established. No pressure dependence could be discerned for reaction 1b between 1.1 and 3.9 atm. A two-parameter, least-squares fit of the current data, valid over the 2253-2975 K temperature range, yields the rate expression k(1b) (cm(3) mol(-1) s(-1)) = 2.24 x 10(15) exp[-41600/T (K)]. Theoretical calculations carried out using a master equation/RRKM analysis fit the measurements reasonably well.
View details for DOI 10.1021/jp0677187
View details for Web of Science ID 000246341200040
View details for PubMedID 17388279
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High-temperature measurements of the rates of the reactions CH2O+Ar -> Products and CH2O+O-2 -> Products
PROCEEDINGS OF THE COMBUSTION INSTITUTE
2007; 31: 175-183
View details for DOI 10.1016/j.proci.2006.07.017
View details for Web of Science ID 000252858000011
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Mesoscale burner Arrays for gas-turbine reheat applications
JOURNAL OF PROPULSION AND POWER
2006; 22 (2): 417-424
View details for Web of Science ID 000236087000015
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Experimental study of confined, swirling, nonpremixed gas flame for validation of simulations
JOURNAL OF PROPULSION AND POWER
2006; 22 (1): 158-168
View details for Web of Science ID 000234910900019
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The reaction of CH3+O-2: experimental determination of the rate coefficients for the product channels at high temperatures
30th International Symposium on Combustion
ELSEVIER SCIENCE INC. 2005: 955–963
View details for DOI 10.1016/j.proci.2004.08.094
View details for Web of Science ID 000229944200102
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Evaluated kinetic data for combustion modeling: Supplement II
JOURNAL OF PHYSICAL AND CHEMICAL REFERENCE DATA
2005; 34 (3): 757-1397
View details for DOI 10.1063/1.1748524
View details for Web of Science ID 000231310600001
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A shock tube study of the reaction NH2+CH4 -> NH3+CH3 and comparison with transition state theory
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
2003; 35 (7): 304-309
View details for DOI 10.1002/kin.10131
View details for Web of Science ID 000183601300004
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A shock tube study of the product branching ratio of the NH2+NO reaction at high temperatures
JOURNAL OF PHYSICAL CHEMISTRY A
2002; 106 (40): 9233-9235
View details for DOI 10.1021/jp020943d
View details for Web of Science ID 000178506700012
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A shock tube study of benzylamine decomposition: Overall rate coefficient and heat of formation of the benzyl radical
JOURNAL OF PHYSICAL CHEMISTRY A
2002; 106 (25): 6094-6098
View details for DOI 10.1021/jp0200851
View details for Web of Science ID 000176356400017
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A shock tube study of the enthalpy of formation of OH
29th International Combustion Symposium
ELSEVIER SCIENCE INC. 2002: 1201–1208
View details for Web of Science ID 000182866100145
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A shock tube study of the NH2+NO2 reaction
29th International Combustion Symposium
ELSEVIER SCIENCE INC. 2002: 2163–2170
View details for Web of Science ID 000182866500090
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Shock tube determination of the overall rate of NH2+NO -> products in the Thermal De-NOx temperature window
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
2001; 33 (11): 715-721
View details for Web of Science ID 000171483200009
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Flow reactor study of the effect of pressure on the thermal De-NOx process
COMBUSTION AND FLAME
2001; 127 (1-2): 1958-1970
View details for Web of Science ID 000172022900007
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Experimental study and modeling of the reaction H+O-2+M -> HO2+M (M = Ar, N-2, H2O) at elevated pressures and temperatures between 1050 and 1250 K
International Discussion Meeting of the Deutsche-Bunsen-Gesellschaft-fur-Physikalische-Chemie
ROYAL SOC CHEMISTRY. 2001: 2337–42
View details for Web of Science ID 000169504900021
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Gas-phase reaction mechanisms for nitrogen oxide formation and removal in combustion
Conference of the NATO-Advanced-Study-Institute on Pollutants from Combustion Formation and Impact on Atmospheric Chemistry
KLUWER ACADEMIC PUBL. 2000: 123–144
View details for Web of Science ID 000166342300007
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Shock tube determination of the overall rate of NH2+NO -> products at high temperatures
28th International Symposium on Combustion
ELSEVIER SCIENCE INC. 2000: 2403–2409
View details for Web of Science ID 000169870400112
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A shock tube study of the product branching ratio for the reaction NH2+NO using frequency-modulation detection of NH2
JOURNAL OF PHYSICAL CHEMISTRY A
1999; 103 (11): 1566-1571
View details for Web of Science ID 000079458500017
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CH-radical concentration measurements in fuel-rich CH4/O-2/Ar and CH4/O-2/NO/Ar mixtures behind shock waves
COMBUSTION AND FLAME
1998; 113 (4): 624-626
View details for Web of Science ID 000073079800016
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An experimental investigation of the effects of compressibility on a turbulent reacting mixing layer
JOURNAL OF FLUID MECHANICS
1998; 356: 25-64
View details for Web of Science ID 000072308800002
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Measurement of the rate coefficient of the reaction CH+O-2->products in the temperature range 2200 to 2600 K
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1997; 29 (10): 781-789
View details for Web of Science ID A1997XX53200007
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Argon broadening of the R(48), R(50) and R(52) lines of CO2 in the (00 degrees 1)<-(00 degrees 0) band
JOURNAL OF QUANTITATIVE SPECTROSCOPY & RADIATIVE TRANSFER
1997; 57 (3): 425-434
View details for Web of Science ID A1997WL78700012
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Argon Broadening of the R (48), R (50) and R (52) Lines of CO2 in the (00°1) ¬ (00°0) Band
Journal of Quantitative Spectroscopy and Radiative Transfer
1997; 57 (3): 425-434
View details for DOI 10.1016/S0022-4073(96)00074-X
- Mechanisms and Modeling of Gas-Phase Aftertreatment Methods for NO Removal from Combustion Products Physical and Chemical Aspects of Combustion edited by Dryer, F., L., Sawyer, R., F. Gordon and Breach. 1997: 29–68
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A shock tube study of CO+OH->CO2+H and HNCO+OH->products via simultaneous laser adsorption measurements of OH and CO2
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1996; 28 (5): 361-372
View details for Web of Science ID A1996UF30600005
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On-line adaptive optimal combustor control
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
1996; 4 (3): 217-229
View details for Web of Science ID A1996UG99100002
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A shock tube study of reactions of CN with HCN, OH, and H-2 using CN and OH laser absorption
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1996; 28 (4): 245-258
View details for Web of Science ID A1996UB30500002
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High-pressure methane oxidation behind reflected shock waves
26th International Symposium on Combustion
COMBUSTION INSTITUTE. 1996: 799–806
View details for Web of Science ID 000083308500095
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Real-time adaptive feedback control of combustion instability
26th International Symposium on Combustion
COMBUSTION INSTITUTE. 1996: 2803–2809
View details for Web of Science ID 000083308500331
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Measurement of the rate coefficient of H+O-2+M -> HO2+M for M = Ar and N-2 at high pressures
26th International Symposium on Combustion
COMBUSTION INSTITUTE. 1996: 481–488
View details for Web of Science ID 000083308500056
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A SHOCK-TUBE STUDY OF METHYL-METHYL REACTIONS BETWEEN 1200 AND 2400 K
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1995; 27 (12): 1179-1196
View details for Web of Science ID A1995TG72500004
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SIMULTANEOUS LASER-ABSORPTION MEASUREMENTS OF CN AND OH IN A SHOCK-TUBE STUDY OF HCN+OH-]PRODUCTS
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1995; 27 (11): 1075-1087
View details for Web of Science ID A1995TB25000004
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MEASUREMENTS OF ARGON COLLISION BROADENING IN THE CN B-2-SIGMA(+)[-X(2)SIGMA(+)(0,0) SPECTRUM
JOURNAL OF QUANTITATIVE SPECTROSCOPY & RADIATIVE TRANSFER
1995; 53 (5): 481-492
View details for Web of Science ID A1995RD79100002
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AN ADAPTIVE OPTIMAL COMBUSTION CONTROL STRATEGY
25th International Symposium on Combustion
ELSEVIER SCIENCE PUBL CO INC. 1995: 101–10
View details for Web of Science ID A1995QG33100012
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Active adaptive control of combustion
4th IEEE Conference on Control Applications
I E E E. 1995: 667–672
View details for Web of Science ID A1995BE48V00118
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On-line combustor performance optimization
Conference on Sensing, Actuation, and Control in Aeropropulsion
SPIE - INT SOC OPTICAL ENGINEERING. 1995: 138–149
View details for Web of Science ID A1995BD37D00012
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Revised Values for the Rate Coefficients of Ethane and Methane Decomposition
International Journal of Chemical Kinetics
1995; 27 (3): 305-308
View details for DOI 10.1002/kin.550270308
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On-line Combustor Performance Optimization
Sensing, actuation, and control in aeropropulsion
1995: 138–49
View details for DOI 10.1117/12.210507
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A Shock Tube Study of Nitric Acid Decomposition
Shock Waves @ Marseille II (Springer-Verlag)
1995: 83-88
View details for DOI 10.1007/978-3-642-78832-1_14
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CO2* chemiluminescence in premixed flames
COMBUSTION SCIENCE AND TECHNOLOGY
1995; 109 (1-6): 183-203
View details for Web of Science ID 000169110500010
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A SHOCK-TUBE STUDY OF THE OH+OH-]H2O+O REACTION
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1994; 26 (4): 389-401
View details for Web of Science ID A1994NC58300001
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Reexamination of Shock-Tube Measurements of the Rate Coefficient of H + O2 -> OH + O
Journal of Physical Chemistry
1994; 98 (17): 4770-4771
View details for DOI 10.1021/j100068a048
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An Experimental Investigation of Supersonic Reacting Mixing Layers
32nd Aerospace Sciences Meeting and Exhibit
1994
View details for DOI 10.2514/6.1994-823
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A STUDY OF ETHANE DECOMPOSITION IN A SHOCK-TUBE USING LASER-ABSORPTION OF CH3
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1993; 25 (11): 969-982
View details for Web of Science ID A1993MC21900008
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DEVELOPMENT OF A CW LASER-ABSORPTION DIAGNOSTIC FOR MEASUREMENT OF CN IN SHOCK-TUBE EXPERIMENTS
JOURNAL OF QUANTITATIVE SPECTROSCOPY & RADIATIVE TRANSFER
1993; 50 (1): 19-34
View details for Web of Science ID A1993LJ39100003
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Compressibility effects in a reacting mixing layer
29th Joint Propulsion Conference and Exhibit
1993
View details for DOI 10.2514/6.1993-1771
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An Experimental Study of the Structure of a Compressible, Reacting Mixing Layer
31st Aerospace Sciences Meeting
1993
View details for DOI 10.2514/6.1993-354
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A SHOCK-TUBE STUDY OF REACTIONS OF ATOMIC OXYGEN WITH ISOCYANIC ACID
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1992; 24 (3): 279-295
View details for Web of Science ID A1992HE02400005
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Control of Combustion-Generated Nitrogen Oxide Emissions: Technology Driven by Regulation
Twenty-Fourth Symposium (International) on Combustion
1992: 859–78
View details for DOI 10.1016/S0082-0784(06)80104-9
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A SHOCK-TUBE STUDY OF H + HNCO -] NH2 + CO
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1991; 23 (8): 655-668
View details for Web of Science ID A1991FX28900001
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A SHOCK-TUBE STUDY OF REACTIONS OF C ATOMS AND CH WITH NO INCLUDING PRODUCT CHANNEL MEASUREMENTS
JOURNAL OF PHYSICAL CHEMISTRY
1991; 95 (8): 3180-3189
View details for Web of Science ID A1991FH09800042
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KINETIC MODELING OF THE REDUCTION OF NITRIC-OXIDE IN COMBUSTION PRODUCTS BY ISOCYANIC ACID
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1991; 23 (4): 289-313
View details for Web of Science ID A1991FF93700002
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A SHOCK-TUBE STUDY OF THE REACTIONS OF NH WITH NO, O2, AND O
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1991; 23 (2): 173-196
View details for Web of Science ID A1991EV72600007
- Chemistry of Gaseous Pollutant Formation and Destruction Fossil Fuel Combustion: A Source Book edited by Bartok, W., Sarofim, A., F. John Wiley. 1991: 215–260
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COMBUSTOR PERFORMANCE ENHANCEMENT THROUGH DIRECT SHEAR-LAYER EXCITATION
COMBUSTION AND FLAME
1990; 82 (1): 75-92
View details for Web of Science ID A1990DZ99200006
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SHOCK-TUBE STUDY OF THE REACTION H + O2-]OH + O USING OH LASER-ABSORPTION
JOURNAL OF PHYSICAL CHEMISTRY
1990; 94 (18): 7119-7128
View details for Web of Science ID A1990DX31800033
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Effects of Controlling Vortex Dynamics on the Performance of a Dump Combustor
Twenty-Third Symposium (International) on Combustion
1990
View details for DOI 10.1016/S0082-0784(06)80369-3
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REACTION-KINETICS OF NH IN THE SHOCK-TUBE PYROLYSIS OF HNCO
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1989; 21 (11): 1049-1067
View details for Web of Science ID A1989AV39800006
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MECHANISM AND MODELING OF NITROGEN CHEMISTRY IN COMBUSTION
PROGRESS IN ENERGY AND COMBUSTION SCIENCE
1989; 15 (4): 287-338
View details for Web of Science ID A1989CJ39700002
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Effect of fuel spray vaporization on the stability characteristics of a dump combustor
25th Joint Propulsion Conference
1989
View details for DOI 10.2514/6.1989-2436
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An Investigation of the Structure of a Laminar Non-Premixed Flame in an Unsteady Vortical Flow
Twenty-Second Symposium (International) on Combustion
1988: 515–22
View details for DOI 10.1016/S0082-0784(89)80058-X
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THE STRUCTURE OF A CHEMICALLY REACTING PLANE MIXING LAYER
JOURNAL OF FLUID MECHANICS
1986; 172: 93-?
View details for Web of Science ID A1986F280600006
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CHEMICAL-KINETICS MODELS FOR COMPLEX REACTING FLOWS
BERICHTE DER BUNSEN-GESELLSCHAFT-PHYSICAL CHEMISTRY CHEMICAL PHYSICS
1986; 90 (11): 934-940
View details for Web of Science ID A1986F382200002
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Soot Production in Axisymmetric Laminar Diffusion Flames at Pressure from One to Ten Atmospheres
Twenty-First Symposium (International) on Combustion
1986: 1115–24
View details for DOI 10.1016/S0082-0784(88)80342-4
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Shock Tube Study of the Reaction between Hydrogen Cyanide and Atomic Oxygen
Twentieth Symposium (International) on Combustion
1985: 647–54
View details for DOI 10.1016/S0082-0784(85)80554-3
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Measurements of the Structure of Sooting Laminar Diffusion Flames at Elevated Pressure
Twentieth Symposium (International) on Combustion
1985: 1035–44
View details for DOI 10.1016/S0082-0784(85)80593-2
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Combustion of Monodisperse Droplet Clouds in a Reactive Environment
Twentieth Symposium (International) on Combustion
1985: 1799–1807
View details for DOI 10.1016/S0082-0784(85)80677-9
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SHOCK-TUBE STUDY OF THE THERMAL-DECOMPOSITION OF CYANOGEN
JOURNAL OF CHEMICAL PHYSICS
1984; 80 (10): 4982-4985
View details for Web of Science ID A1984SS95800048
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HIGH-TEMPERATURE DETERMINATION OF THE RATE COEFFICIENT FOR THE REACTION H2O+CN-]HCN+OH
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1984; 16 (12): 1609-1621
View details for Web of Science ID A1984AAA2500013
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HIGH-TEMPERATURE DETERMINATION OF THE RATE COEFFICIENT FOR THE REACTION H2+CN-]H+HCN
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1983; 15 (9): 915-923
View details for Web of Science ID A1983RH56700006
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Shock Tube Determination of the Rate Coefficient for the Reaction CN+HCN → C2N2+H
INTERNATIONAL JOURNAL OF CHEMICAL KINETICS
1983; 15 (11): 1237-1241
View details for DOI 10.1002/kin.550151110
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A Three-Zone Model for Coal Particle Swelling
Combustion Science and Technology
1983; 31: 195-201
View details for DOI 10.1080/00102208308923640
- Shock Tube Study of the Thermal Decomposition of Hydrogen Cyanide Shock Tubes and Waves 1981
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SHOCK-TUBE MEASUREMENTS OF RATE COEFFICIENTS OF ELEMENTARY GAS REACTIONS
JOURNAL OF PHYSICAL CHEMISTRY
1979; 83 (6): 757-763
View details for Web of Science ID A1979GN84300023
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Effects of Inlet Air Swirl and Fuel Volatility on the Structure of Confined Spray Flames
Seventeenth Symposium (International) on Combustion
1979: 467–73
View details for DOI 10.1016/S0082-0784(79)80047-8
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Alternative Hydrocarbon Fuels: Combustion and Chemical Kinetics
AIAA Progress in Astronautics and Aeronautics
edited by Bowman, C. T.
AIAA, New York. 1978; 62
View details for DOI 10.2514/4.865367
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Pollutant Formation and Energy Release in Confined Turbulent Diffusion Flames
Sixteenth Symposium (International) on Combustion
1977: 105–17
View details for DOI 10.1016/S0082-0784(77)80317-2
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Probe Measurements in Flames
Experimental Diagnostics in Gas Phase Combustion Systems
edited by Bowman, C. T., Price, E. W., Skifstad, J. G., Zinn, B. T., Hartley, D. L.
AIAA. 1977: 3–24
View details for DOI 10.2514/5.9781600865275.0003.0024
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Pollutant formation and energy release in liquid-fuel turbulent diffusion flames
15th Aerospace Sciences Meeting
1977
View details for DOI 10.2514/6.1977-53
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Kinetics of Thermal Decomposition of Hydrogen Sulfide behind Shock Waves
Sixteenth Symposium (International) on Combustion
1977: 971–82
View details for DOI 10.1016/S0082-0784(77)80389-5
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Kinetics of Pollutant Formation and Destruction in Combustion
Progress in Energy and Combustion Science
1975; 1 (1): 33-45
View details for DOI 10.1016/0360-1285(75)90005-2
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A Shock Tube Investigation of the High-Temperature Oxidation of Methanol
Combustion and Flame
1975; 25: 343-354
View details for DOI 10.1016/0010-2180(75)90106-6
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Non-Equilibrium Radical Concentrations in Shock-Initiated Methane Oxidation
Fifteenth Symposium (International) on Combustion
1975: 869–82
View details for DOI 10.1016/S0082-0784(75)80354-7
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Comment on “molecular beam sampling of H2CO and NO in one-atmosphere methaneair flames”
Combustion and Flame
1975; 25: 397-398
View details for DOI 10.1016/0010-2180(75)90113-3
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Kinetics of Nitric Oxide Formation in Combustion Processes
Fourteenth Symposium (International) on Combustion
1973: 729–38
View details for DOI 10.1016/S0082-0784(73)80068-2
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Investigation of Nitric Oxide Formation Kinetics in Combustion Processes: The Hydrogen-Oxygen-Nitrogen Reaction
Combustion Science and Technology
1971; 3 (1): 37-45
View details for DOI 10.1080/00102207108952269
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An Experimental and Analytical Study of Methane Oxidation behind Shock Waves
Combustion and Flame
1970; 14 (1): 37-47
View details for DOI 10.1016/S0010-2180(70)80008-6
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An Experimental and Analytical Investigation of the High-Temperature Oxidation Mechanisms of Hydrocarbon Fuels
Combustion Science and Technology
1970; 2: 161-172
View details for DOI 10.1080/00102207008952244
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Vibrational Relaxation of HCl behind Shock Waves
J. Chem. Phys.
1969; 50: 1904-1905
View details for DOI 10.1063/1.1671298
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Dissociation of HCl behind Shock Waves
J. Chem. Phys.
1968; 48: 4314-4317
View details for DOI 10.1063/1.1669776
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Chemiluminescence in the High-Temperature Oxidation of Methane
Combustion and Flame
1968; 12: 611-614
View details for DOI 10.1016/0010-2180(68)90080-1
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Combustion Instability in Gas Rockets
AIAA J.
1965; 3: 1981-1982
View details for DOI 10.2514/3.55206
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A Shock Tube Study of the Reactions of NCO with O and NO using NCO Laser Absorption
Twenty-Fourth Symposium (International) on Combustion
1992: 701–710
View details for DOI 10.1016/S0082-0784(06)80086-X
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A Shock Tube Study of the Reaction of CN and NCO with NO2
Twenty-Fifth Symposium (International) on Combustion
1994: 983–991
View details for DOI 10.1016/S0082-0784(06)80735-6
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A Shock Tube Study of Methane Decomposition Using Laser Absorption by CH3
Twenty-Fourth Symposium (International) on Combustion
1992: 589–596
View details for DOI 10.1016/S0082-0784(06)80072-X
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High Temperature Shock Tube Study of Reactions of CH and C-Atoms with N2
Twenty-Third Symposium (International) on Combustion
1990: 259–265
View details for DOI 10.1016/S0082-0784(06)80268-7
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A Shock Tube Study of the CO+OH → CO2+H Reaction
Twenty-Fifth Symposium (International) on Combustion
1994: 741–748
View details for DOI 10.1016/S0082-0784(06)80706-X