High-Pressure Kinetic Mechanisms for Hydrogen and Hydrogen Syngas
|
|
- Grace Glenn
- 5 years ago
- Views:
Transcription
1 High-Pressure Kinetic Mechanisms for Hydrogen and Hydrogen Syngas 1 st International Workshop on Flame Chemistry Warsaw, Poland July 28, 212 Michael P. Burke Chemical Sciences and Engineering Division, Argonne National Laboratory Frederick L. Dryer Department of Mechanical and Aerospace Engineering, Princeton University Other collaborators: Yiguang Ju, Marcos Chaos, Jeffrey Santner, Francis M. Haas Stephen Klippenstein, Lawrence Harding
2 Motivation Growing interest in computational engine design/testing Fluid mechanics and kinetics sub-models H 2 and H 2 /CO Synthesis gas (H 2 /CO/H 2 O/CO 2 ) from coal/biomass gasification Core sub-model for all fuels Advanced engine technologies High P, low T f Modeling difficulties for flames Mass burning rate (g cm -2 s -1 ) C 2 H 2 /air, φ=.43 T f ~ 16K (Shi & Reitz 21) USC-MECH II USC-MECH II with Davis H2 Subset USC-MECH II with GRI 3. H2 Subset Pressure (atm) (Burke et al. 211) Y. Shi, R.D. Reitz, Fuel 89 (21) M.P. Burke, M. Chaos, F.L. Dryer, Y. Ju, Combustion and Flame 157 (21) M.P. Burke, F.L. Dryer, Y. Ju, Proceedings of the Combustion Institute 33 (211)
3 Difficulty in predicting high-pressure flames Mass burning rate (g cm -2 s -1 ) H 2 /O 2 /He, φ=.85 T f ~16K Present experiments Tse et al. (2) Konnov (28) Li et al. (27) Saxena & Williams (26) Sun et al. (27) O'Connaire et al. (24) Davis et al. (25) GRI-MECH 3. (1999) Pressure (atm) Mass burning rate (g cm -2 s -1 ) H 2 /O 2 /Ar, φ=2.5 T f ~16K Present experiments Li et al. (27) O'Connaire et al. (24) Saxena & Williams (26) Davis et al. (25) Konnov (28) Sun et al. (27) GRI-MECH 3. (1999) Pressure (atm) Large variations among models None of the models capture pressure dependence across all conditions M.P. Burke, M. Chaos, F.L. Dryer, Y. Ju, Combustion and Flame 157 (21) M.P. Burke, F.L. Dryer, Y. Ju, Proceedings of the Combustion Institute 33 (211)
4 H mole fraction What controls high-p/low-t f flames? 1 atm 1 atm 2 atm Temperature (K) HO 2+O=O 2+OH HO 2+HO 2=H 2O 2+O 2 O+H 2 =H+OH HO 2+H=OH+OH HO 2+OH=H 2O+O 2 H 2+OH=H 2O+H H+O 2 =O+OH H+O 2(+M)=HO 2(+M) Sensitivity Coefficient H 2 /O 2 /He, φ=.3 T f ~14K 1 atm 5 atm 1 atm Flux (mole/cm 3 /s) H+O 2 M.P. Burke, M. Chaos, F.L. Dryer, Y. Ju, Combustion and Flame 157 (21) M.P. Burke, F.L. Dryer, Y. Ju, Proceedings of the Combustion Institute 33 (211) OH+O (R1) +M HO 2 (R2) increasing P More HO 2 more HO 2 +radical flux Flame zone shifts peak sensitivity at higher T s collision efficiencies of products More R1/R2 competition amplified sensitivity (Situation similar for H 2 /CO) 4
5 Complexity of the modeling problem HO 2 +O=O 2 +OH HO 2 +HO 2 =H 2 O 2 +O 2 O+H 2 =H+OH HO 2 +H=OH+OH HO 2 +OH=H 2 O+O 2 H 2 +OH=H 2 O+H H+O 2 =O+OH H+O 2 (+M)=HO 2 (+M) Sensitivity Coefficient H 2 /O 2 /He, φ=.3 T f ~14K 1 atm 5 atm 1 atm Uncertainty in all reactions of 1% burning rate uncertainty of 3% Realistic accuracy improvements for elementary reactions will not yield typical expected accuracies for global behavior Optimization against global targets necessary Mass burning rate (g cm -2 s -1 ) H 2 /O 2 /He, φ=.5, T f ~ 14K Li et al. Li et al. w/ (R7) Fit 1 Li et al. w/ (R7) Fit 2 OH+HO 2 =H 2 O+O Pressure (atm) Functional temperature dependence of OH+HO 2 =H 2 O+O 2 highly disputed/ unknown Parameter optimization techniques don t work if the functional dependence is not known 1. M.P. Burke, F.L. Dryer, Y. Ju, Proceedings of the Combustion Institute 33 (211)
6 Complexity of the modeling problem HO 2 +O=O 2 +OH HO 2 +HO 2 =H 2 O 2 +O 2 O+H 2 =H+OH HO 2 +H=OH+OH HO 2 +OH=H 2 O+O 2 H 2 +OH=H 2 O+H H+O 2 =O+OH H+O 2 (+M)=HO 2 (+M) Sensitivity Coefficient H 2 /O 2 /He, φ=.3 T f ~14K 1 atm 5 atm 1 atm Mass burning rate (g cm -2 s -1 ) H 2 /O 2 /He, φ=.5, T f ~ 14K Li et al. Li et al. w/ (R7) Fit 1 Li et al. w/ (R7) Fit 2 OH+HO 2 =H 2 O+O Pressure (atm) A rigorous modeling solution will likely require both: Empirical adjustments to rate constants Improved fundamental understanding of select processes Neither alone appears sufficient to solve the problem. 1. M.P. Burke, F.L. Dryer, Y. Ju, Proceedings of the Combustion Institute 33 (211)
7 Updated kinetic-transport models H 2 : Hong et al. (211) and Burke et al. (212)* HO 2 formation/consumption H+O 2 (+M) = HO 2 (+M) HO 2 +radical reactions H 2 O 2 reactions among others CO: Haas et al. (212) CO + OH = CO 2 + H, CO + HO 2 = CO 2 + OH HCO chemistry *Uncertainties remained: adjustments of rate parameters to improve predictions Z. Hong, D.F. Davidson, R.K. Hanson, Combust. Flame 158 (211) M.P. Burke, M. Chaos, Y. Ju, F.L. Dryer, S.J. Klippenstein, Int. J. Chem. Kinet. 44 (212) F.M. Haas, S. Vranckx, M. Chaos, R.X. Fernandes, F.L. Dryer (212) in preparation. 7
8 Model performance [O 2 ] τ ig (mol liter -1 µs) OH mole fraction (ppm) Skinner and Ringrose (1965) - 5 atm Schott and Kinsey (1958) - 1 atm Petersen et al. (1995) - 33 atm Petersen et al. (1995) - 64 atm Petersen et al. (1995) - 57 & 87 atm Present model Hong et al. 1/T (K -1 ) Hong et al. (21) Present model -.7ppm H Present model -.7ppm H, +/- 23K Hong et al. -.7ppm H Mass burning rate (g cm -2 s -1 ).25 a) φ =.7 Burke et al. (21, 211) b) φ = 1. c) φ = 2.5 Present model Hong et al. Burke et al. (212) Haas et al. (212) Time (ms) Pressure (atm) (Santer et al. 212, 5E1 on Friday) Hong/Burke perform similarly well against most targets Largest differences in flames Burke et al. within 2%, Hong et al. within 4% Parameter adjustments not unique uncertainties remain! Z. Hong, D.F. Davidson, R.K. Hanson, Combust. Flame 158 (211) M.P. Burke, M. Chaos, Y. Ju, F.L. Dryer, S.J. Klippenstein, Int. J. Chem. Kinet. 44 (212) F.M. Haas, S. Vranckx, M. Chaos, R.X. Fernandes, F.L. Dryer (212) in preparation. J. Santner, F.L. Dryer, Y. Ju, Proc. Combust. Inst. (212) in press, oral presentation : 5E1 on Friday. 8
9 Uncertainties remaining in 212 (for flames) Parametric uncertainties HO 2 + X reactions HO 2 + H = OH + OH H2 + O 2 H 2 O + O HO 2 + OH = H 2 O + O 2 HO 2 + HO 2 = H 2 O 2 + O 2 H + O 2 (+M) = HO 2 (+M) Pressure dependence 3 rd body efficiencies for H 2 O and CO 2 CO + O + M = CO 2 + M Model assumptions Nonlinear mixture rules M.P. Burke, M. Chaos, Y. Ju, F.L. Dryer, S.J. Klippenstein, Int. J. Chem. Kinet. 44 (212) F.M. Haas, S. Vranckx, M. Chaos, R.X. Fernandes, F.L. Dryer (212) in preparation. P. Saxena, F.A. Williams, 7th US National Combustion Meeting, Atlanta, GA,
10 Recall the complexity of the modeling problem and uncertainties in OH+HO 2 = H 2 O+O 2 HO 2 +O=O 2 +OH HO 2 +HO 2 =H 2 O 2 +O 2 O+H 2 =H+OH HO 2 +H=OH+OH HO 2 +OH=H 2 O+O 2 H 2 +OH=H 2 O+H H+O 2 =O+OH H+O 2 (+M)=HO 2 (+M) Sensitivity Coefficient H 2 /O 2 /He, φ=.3 T f ~14K 1 atm 5 atm 1 atm Mass burning rate (g cm -2 s -1 ) H 2 /O 2 /He, φ=.5, T f ~ 14K Li et al. Li et al. w/ (R7) Fit 1 Li et al. w/ (R7) Fit 2 OH+HO 2 =H 2 O+O Pressure (atm) A rigorous modeling solution will likely require both: Empirical adjustments to rate constants Improved fundamental understanding of select processes Neither alone appears sufficient to solve the problem. 1. M.P. Burke, F.L. Dryer, Y. Ju, Proceedings of the Combustion Institute 33 (211)
11 Modeling strategies Current kinetic models: sets of rate parameters Hierarchical, comprehensive modeling Westbrook & Dryer (1984) Optimization and Uncertainty Quantification Frenklach (1984), Frenklach,Wang,Rabinowitz (1992):Solution-mapping + optimization of A-factors Frenklach et al. (24), Sheen & Wang (29): Uncertainty Quantification of A-factors Turányi et al. (212), Sheen et al. (212): Uncertainty quantification of A-n-E a Require massive amounts of data to constrain full T/P/M-dependence of all k s Extrapolation outside the dataset very challenging Direct incorporation of theory useful Replaces fitting formulas with physical theories Common for extrapolation of data for a single reaction Imposes constraints spanning all T/P/M Multi-scale models: sets of molecular parameters Optimal use of information from ab initio calculations, k measurements, combustion measurements Theory fills in the gaps across all T/P/M 1. M.P. Burke, S.J. Klippenstein, L.B. Harding, Proceedings of the Combustion Institute (212) in press. 11
12 OH + HO 2 = H 2 O + O k (cm 3 mol -1 s -1 ) 1 13 OH + HO 2 = H 2 O + O 2 (R1) H 2 O 2 (+M) = OH+OH(+M) (R2) H 2 O 2 +OH = HO 2 +H 2 O (R3) HO 2 +HO 2 = H 2 O 2 +O 2 (R4) HO 2 +OH = H 2 O+O 2 (R5) OH+OH = O+H 2 O Peeters and Mahnen (1973) DeMore (1979) Lii et al. (198) Cox et al. (1981) Kurylo et al. (1981) Braun et al. (1982) DeMore (1982) Goodings & Hayhurst (1988) Keyser (1988) Hippler & Troe (1992) 1/T (K -1 ) Hippler et al. (1995) Kappel et al. (22) Srinivasan et al. (26) Hong et al. (21) Keyser (1988) Sivaramakarishnan et al. (27) Chaos & Dryer (28) - Hippler Chaos & Dryer (28) - Kappel Rasmussen et al. (28) Mass burning rate (g cm -2 s -1 ) H 2 /O 2 /He, φ=.5, T f ~ 14K Li et al. Li et al. w/ (R7) Fit 1 Li et al. w/ (R7) Fit Pressure (atm) 12
13 Multi-scale informatics set of molecular parameters informed by data across all scales I. Molecular data E, v s, v imag, TST, RRKM-ME, II. Rate constant measurements k n (T,P,M) -D reactor, 1-D flame, III. Combustion measurements [OH] vs. t,s u, Mathematical implementation (I) + (IV) Local surrogate model Least-squares error minimization Iterated until converged Sij = δ ij X = Optimization parameters: Molecular parameters + experimental conditions E, v s, v imag, + T, P, [M i ], F ( X ) ± Z i j = Yt, i i (II) (III) S ij = n S ij lnk ln k p, n ( Ti, Pi, M i ) = X p, n Fi ( T, P, M ) i i i j lnk p, n ( T, P, M ) i X j i i ~ S = Y ± ij ( X j X j ) j i Z i X j,opt and C X 13
14 Implementation for H 2 O 2 system Optimization variables H 2 O 2 (+M) = OH+OH(+M) A' (1), n (1), E (1) H 2 O 2 +OH = HO 2 +H 2 O E (2), v' all(2), v' tr(2), v' ss(2), v' imag(2), E w(2), η' H2O2, η' TS(2) 1 14 OH + HO 2 = H 2 O + O 2 HO 2 +HO 2 = H 2 O 2 +O 2 HO 2 +OH = H 2 O+O 2 OH+OH = O+H 2 O Shock-heated H 2 O 2 /H 2 O/O 2 /Ar Shock-heated H 2 O/O 2 /Ar Shock-heated H 2 O 2 /Ar Optimization Targets E (3), v' all(3), v' tr(3), v' ss(3), v' imag(3), E w(3), η' TS(3) E (4g), v' all(4), v' tr(4g), v' ss(4g), v' imag(4g), E w(4g), η' TS(4g) E (4e), v' TS(4e), v' tr(4e), v' ss(4e), η' TS(4e), f ' VRCTST,c(4) E (5g), v' all(5), v' tr(5g), v' ss(5g), v' imag(5g), E w(5g) E (5e), v' TS(5e), v' tr(5e), v' ss(5e) T' i, P' i, M' H2O2,o,i, M' H2O,o,i, M' O2,o,i T' i, P' i, M' H2O,o,i, M' O2,o,i, M' H,o,i T' i, P' i, M' H2O2,o,i, σ' 1,H2O2, σ' 2,H2O2, σ' 1,HO2, σ' 2,HO2 I. Molecular data: ab initio calculations (Klippenstein/Harding) II. Rate constant measurements: see paper III. Combustion measurements: OH(t), H 2 O(t) Shock-heated H 2 O 2 /Ar (Hong et al. 29,21) OH(t) Shock-heated H 2 O/O 2 /Ar (Hong et al. 21) abs 215nm (t) Shock-heated H 2 O 2 /Ar (Kappel et al. 22) k (cm 3 mol -1 s -1 ) 1 13 DeMore (198) DeMore (1982) Keyser (1988) Lii et al. (198) Cox et al. (1981) Kurylo et al. (1981) Braun et al. (1982) 1. M.P. Burke, S.J. Klippenstein, L.B. Harding, Proceedings of the Combustion Institute (212) in press. Kappel et al. (22) Srinivasan et al. (26) Hong et al. (21) T (K),, 14
15 Different interpretations for OH+HO Absorbance (a) Kappel et al. experiments Kappel et al. predictions A priori model Optimized Constrained model (b) Kappel et al. (22) (c) Much weaker T-dependence (Secondary reactions) Time (ms) Mole fraction (ppm) Hong et al. experiments Hong et al. predictions A priori model Constrained model Hong et al. (21) Time (ms) Lower magnitude (Arbitrary H atom doping) 1. M.P. Burke, S.J. Klippenstein, L.B. Harding, Proceedings of the Combustion Institute (212) in press. 15
16 Absorbance Mole fraction (ppm) Consistent description of OH+HO 2 = H 2 O+O 2 Kappel et al. experiments Kappel et al. predictions A priori model Optimized Constrained model Time (ms) Hong et al. experiments Hong et al. predictions A priori model Constrained model (a) (b) Kappel et al. (22) (c) Hong et al. (21) Time (ms) k (cm 3 mol -1 s -1 ) DeMore (198) DeMore (1982) Keyser (1988) Lii et al. (198) Cox et al. (1981) Kurylo et al. (1981) Braun et al. (1982) Kappel et al. (22) Srinivasan et al. (26) Hong et al. (21) A priori model Constrained model T (K) Single description consistent with: 1. Ab initio calculations 2. Low-T k measurements 3. High-T raw global data Milder T-dependence Minimum near 12 K 1. M.P. Burke, S.J. Klippenstein, L.B. Harding, Proceedings of the Combustion Institute (212) in press. 16
17 Absorbance Mole fraction (ppm) Consistent description of OH+HO 2 = H 2 O+O 2 Kappel et al. experiments Kappel et al. predictions A priori model Optimized Constrained model Time (ms) Hong et al. experiments Hong et al. predictions A priori model Constrained model (a) (b) Kappel et al. (22) (c) Hong et al. (21) Time (ms) k (cm 3 mol -1 s -1 ) Simultaneous weighting of diverse data types DeMore (198) DeMore (1982) Keyser (1988) Lii et al. (198) Cox et al. (1981) Kurylo et al. (1981) Braun et al. (1982) Kappel et al. (22) Srinivasan et al. (26) Hong et al. (21) A priori model Constrained model T (K) Theory guides experimental interpretations Raw data and careful documentation extremely powerful 1. M.P. Burke, S.J. Klippenstein, L.B. Harding, Proceedings of the Combustion Institute (212) in press. 17
18 Absorbance Mole fraction (ppm) Consistent description of OH+HO 2 = H 2 O+O 2 Kappel et al. experiments Kappel et al. predictions A priori model Optimized Constrained model Time (ms) Hong et al. experiments Hong et al. predictions A priori model Constrained model Time (ms) (a) (b) Kappel et al. (22) (c) Hong et al. (21) k (cm 3 mol -1 s -1 ) DeMore (198) DeMore (1982) Keyser (1988) Lii et al. (198) Cox et al. (1981) Kurylo et al. (1981) Braun et al. (1982) Hong et al. (212) Kappel et al. (22) Srinivasan et al. (26) Hong et al. (21) A priori model Constrained model T (K) Z. Hong, K.-Y. Lam, R. Sur, S. Wang, D.F. Davidson, R.K. Hanson On the rate constants of OH + HO 2 and HO 2 + HO 2 : A comprehensive study of H 2 O 2 thermal decomposition using multi-species laser absorption. Combustion Symposium: 5D11 M.P. Burke, S.J. Klippenstein, L.B. Harding A quantitative explanation for the apparent anomalous temperature dependence of OH + HO 2 = H 2 O + O 2 through multi-scale modeling. Combustion Symposium: 4D9 M.P. Burke, S.J. Klippenstein, L.B. Harding, Proceedings of the Combustion Institute (212) in press. Z. Hong, K.-Y. Lam, R. Sur, S. Wang, D.F. Davidson, R.K. Hanson, Proc Combust Inst (212) in press.,, 18
19 Conclusions High-pressure syngas flames Emphasize HO 2 pathways + collision efficiencies of CO 2 /H 2 O Inherently difficult to model Rigorous modeling solutions Empirical adjustments based on global targets Improved fundamental characterization Uncertainties remain in both 1) model parameters and 2) model assumptions Moving forward Incorporation of theory to fill in the gaps Raw data and careful documentation Characterization of non-idealities/uncertainties in experiments and theory 19
20 Acknowledgements This work was supported by: Director s Postdoctoral Fellowship from Argonne National Laboratory (MPB) U. S. Department of Energy, Office of Basic Energy Sciences under Contract No. DE-AC2-6CH11357 (SJK, LBH) U. S. Department of Energy, University Turbine Systems Research Program under Contract No. DE-NT752 (FLD,YJ) U.S. Department of Energy, Office of Basic Energy Sciences, Energy Frontier Research Center under Contract No. DE- SC1198 (FLD,YJ) 2
21 Thank you. Questions? 21
22 End 22
Hierarchical approach
Chemical mechanisms Examine (i) ways in which mechanisms are constructed, (ii)their dependence on rate and thermodynamic data and (iii) their evaluation using experimental targets Copyright 2011 by Michael
More informationSimplified Chemical Kinetic Models for High-Temperature Oxidation of C 1 to C 12 n-alkanes
Simplified Chemical Kinetic Models for High-Temperature Oxidation of C 1 to C 1 n-alkanes B. Sirjean, E. Dames, D. A. Sheen, H. Wang * Department of Aerospace and Mechanical Engineering, University of
More informationTopic 6 Chemical mechanisms
Topic 6 Chemical mechanisms Examine ways in which mechanisms are constructed, their dependence on rate and thermodynamic data, their evaluation using experimental targets and the optimization of component
More informationFundamental Kinetics Database Utilizing Shock Tube Measurements
Fundamental Kinetics Database Utilizing Shock Tube Measurements Volume 6: Reaction Rate Measurements (January 2009 to January 2014) D. F. Davidson and R. K. Hanson Mechanical Engineering Department Stanford
More informationConfirmation of paper submission
www.flame-structure-2014.com Berlin Institute of Technology (TU Berlin) Prof. Dr. Frank Behrendt Fakultät III: Prozesswissenschaften, Institut für Energietechnik Chair Energy Process Engineering and Conversion
More informationA REDUCED-ORDER METHANE-AIR COMBUSTION MECHANISM THAT SATISFIES THE DIFFERENTIAL ENTROPY INEQUALITY
THE PUBLISHING HOUSE PROCEEDINGS OF THE ROMANIAN ACADEMY, Series A, OF THE ROMANIAN ACADEMY Special Issue/2018, pp. 285 290 A REDUCED-ORDER METHANE-AIR COMBUSTION MECHANISM THAT SATISFIES THE DIFFERENTIAL
More informationStudies of pyrolysis and oxidation of methyl formate using molecular beam mass spectrometry
Paper 070RK-0168 0168 Topic: Reaction Kinetics 8 th U. S. National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22,
More informationTheoretical Gas Phase Chemical Kinetics. Stephen J. Klippenstein
Theoretical Gas Phase Chemical Kinetics Stephen J. Klippenstein Goal Contribute to Improving the Accuracy of Mechanisms Theoretical Kinetics Predictions for Key Reactions Guided by Modeling Efforts Butanol
More informationMulti-scale Informatics for Low-Temperature Propane Oxidation
Paper # 070RK-0169 Topic: Reaction Kinetics 8 th U. S. National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013
More informationModeling and Simulation of Plasma-Assisted Ignition and Combustion
Modeling and Simulation of Plasma-Assisted Ignition and Combustion Vigor Yang and Sharath Nagaraja Georgia Institute of Technology Atlanta, GA AFOSR MURI Fundamental Mechanisms, Predictive Modeling, and
More informationDynamics of Excited Hydroxyl Radicals in Hydrogen Based Mixtures Behind Reflected Shock Waves. Supplemental material
Dynamics of Excited Hydroxyl Radicals in Hydrogen Based Mixtures Behind Reflected Shock Waves Proceedings of the Combustion Institute 34, 22 Supplemental material R. MÉVEL, S. PICHON, L. CATOIRE, N. CHAUMEIX,
More informationPremixed MILD Combustion of Propane in a Cylindrical. Furnace with a Single Jet Burner: Combustion and. Emission Characteristics
Premixed MILD Combustion of Propane in a Cylindrical Furnace with a Single Jet Burner: Combustion and Emission Characteristics Kin-Pang Cheong a, c, Guochang Wang a, Jianchun Mi a*, Bo Wang a, Rong Zhu
More informationHigh Pressure Single Pulse Shock Tube (HPST) Experiments
High Pressure Single Pulse Shock Tube (HPST) Experiments Kenneth Brezinsky Mechanical Engineering University of Illinois, Chicago 27 AFOSR MURI Kick-Off Meeting Generation of Comprehensive Surrogate Kinetic
More informationFlame Chemistry and Diagnostics
Flame Chemistry and Diagnostics High-Temperature Oxidation of (1) n-butanol and (2) C 4 - Hydrocarbons in Low-Pressure Premixed Flames Nils Hansen, Michael R. Harper, William H. Green Bin Yang, Hai Wang,
More informationCombustion Chemistry of a New Biofuel: Butanol
Combustion Chemistry of a New Biofuel: Butanol William H. Green, D.F. Davidson, F. Egolfopoulos, N. Hansen, M. Harper, R.K. Hanson, S. Klippenstein, C.K. Law, C.J. Sung, D.R. Truhlar, & H. Wang Assessing
More informationKinetics of the Reactions of H and CH 3 Radicals with nbutane: An Experimental Design Study using Reaction Network Analysis
Paper # 070RK-0277 Topic: Reaction Kinetics 8 th U. S. National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013
More informationInvestigation of ethane pyrolysis and oxidation at high pressures using global optimization based on shock tube data
Investigation of ethane pyrolysis and oxidation at high pressures using global optimization based on shock tube data Viktor Samu 1, Tamás Varga 1,2, Tamás Turányi 1 1 Institute of Chemistry, Eötvös University
More informationPredictive Theoretical Elementary Reaction Kinetics and its Role in Combustion Modeling. Stephen J. Klippenstein
Predictive Theoretical Elementary Reaction Kinetics and its Role in Combustion Modeling Stephen J. Klippenstein Theoretical Elementary Reaction Kinetics Potential Energy Surface Exploration Ab Initio Electronic
More informationPostdoctoral Scholar Hanson Research Group, Mechanical Engineering, Stanford University, CA
SHENGKAI WANG EDUCATION Phone: +1 (650) 391-6853 Email: sk.wang@stanford.edu Address: 418 Panama Mall, Rm. 106 Stanford, CA, 94305 Ph.D. in Mechanical Engineering, Stanford University, Stanford, CA 01/2017
More informationCombustion Chemistry
Combustion Chemistry Hai Wang Stanford University 2015 Princeton-CEFRC Summer School On Combustion Course Length: 3 hrs June 22 26, 2015 Copyright 2015 by Hai Wang This material is not to be sold, reproduced
More informationChemical Kinetics of Combustion Processes
2010 CEFRC Conference Chemical Kinetics of Combustion Processes Hai Wang B. Yang, J. Camacho, S. Lieb, S. Memarzadeh, S.-K. Gao and S. Koumlis University of Southern California Benzene + O( 3 P) Products
More informationMichael P. Burke PROFESSIONAL EXPERIENCE EDUCATION AND TRAINING AWARDS AND RECOGNITIONS
Michael P. Burke 228 Mudd Building, Mail Code 4703 mpburke@columbia.edu Columbia University 212-851-0782 500 W. 120th Street http://burke.me.columbia.edu/ New York, NY 10027 PROFESSIONAL EXPERIENCE Columbia
More informationPressure and preheat dependence of laminar flame speeds of H 2 /CO/CO 2 /O 2 /He mixtures
Available online at www.sciencedirect.com Proceedings of the Combustion Institute 32 (2009) 1261 1268 Proceedings of the Combustion Institute www.elsevier.com/locate/proci Pressure and preheat dependence
More informationDevelopment and Optimization of H 2 /CO-H 2 Reaction Model using
Development and Optimization of H 2 /CO-H 2 Reaction Model using PrIMe A. Mirzayeva 1, N.A. Slavinskaya 1, U. Riedel 1, M. Frenklach 2, A. Packard 2, W. Li 2, J. Oreluk 2, A. Hedge 2 1 Institute of Combustion
More informationSupersonic Combustion Simulation of Cavity-Stabilized Hydrocarbon Flames using Ethylene Reduced Kinetic Mechanism
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 9-12 July 2006, Sacramento, California AIAA 2006-5092 Supersonic Combustion Simulation of Cavity-Stabilized Hydrocarbon Flames using Ethylene
More informationA5-stepreducedmechanismforcombustionof CO/H 2 /H 2 O/CH 4 /CO 2 mixtures with low hydrogen/methane and high H 2 Ocontent
A5-stepreducedmechanismforcombustionof CO/H 2 /H 2 O/CH 4 /CO 2 mixtures with low hydrogen/methane and high H 2 Ocontent Z. M. Nicolaou a, J. Y. Chen b, N. Swaminathan a a Cambridge University, Department
More informationTHE ROLE OF SENSITIVITY ANALYSIS IN MODEL IMPROVEMENT
Energy and Resources Research Institute School of something FACULTY OF OTHER Faculty of Engineering THE ROLE OF SENSITIVITY ANALYSIS IN MODEL IMPROVEMENT Alison S. Tomlin Michael Davis, Rex Skodje, Frédérique
More informationCorrelations for the ignition delay times of hydrogen/air mixtures
Article Engineering Thermophysics January 20 Vol.56 No.2: 25 22 doi: 0.007/s434-00-4345-3 SPECIAL TOPICS: Correlations for the ignition delay times of hydrogen/air mixtures ZHAO ZhenLong, CHEN Zheng *
More informationKinetic Modeling of Methyl Formate Oxidation
7 th US National Technical Meeting of the Combustion Institute Hosted by the Georgia Institute of Technology, Atlanta, GA March 20 23, 2011 Kinetic Modeling of Methyl Formate Oxidation Richard H. West
More informationThis paper is part of the following report: UNCLASSIFIED
UNCLASSIFIED Defense Technical Information Center Compilation Part Notice ADP023624 TITLE: Ignition Kinetics in Fuels Oxidation DISTRIBUTION: Approved for public release, distribution unlimited This paper
More informationCOMBUSTION OF THE BUTANOL ISOMERS: REACTION PATHWAYS AT ELEVATED PRESSURES FROM LOW-TO-HIGH TEMPERATURES
COMBUSTION OF THE BUTANOL ISOMERS: REACTION PATHWAYS AT ELEVATED PRESSURES FROM LOW-TO-HIGH TEMPERATURES Michael R. Harper, William H. Green* Massachusetts Institute of Technology, Department of Chemical
More informationExperimental and modeling study of the pyrolysis and combustion of dimethoxymethane
Experimental and modeling study of the pyrolysis and combustion of dimethoxymethane Florence Vermeire, Hans-Heinrich Carstensen, Olivier Herbinet, Frédérique Battin-Leclerc, Guy B. Marin and Kevin M. Van
More informationMichael P. Burke PROFESSIONAL EXPERIENCE EDUCATION AND TRAINING AWARDS AND RECOGNITIONS
Michael P. Burke 228 Mudd Building, Mail Code 4703 mpburke@columbia.edu Columbia University 212-851-0782 500 W. 120th Street http://burke.me.columbia.edu/ New York, NY 10027 PROFESSIONAL EXPERIENCE Columbia
More informationAssessment of existing H 2 /O 2 chemical reaction mechanisms at reheat gas turbine conditions
international journal of hydrogen energy 36 (2011) 12025e12034 Available at www.sciencedirect.com journal homepage: www.elsevier.com/locate/he Assessment of existing H 2 /O 2 chemical reaction mechanisms
More informationIgnition Delay Time of Small Hydrocarbons-Nitrous Oxide(-Oxygen) Mixtures
24 th ICDERS July 28 - August 2, 2013 Taipei, Taiwan Ignition Delay Time of Small Hydrocarbons-Nitrous Oxide(-Oxygen) Mixtures Rémy Mével and Joseph Shepherd Graduate Aerospace Laboratories, California
More informationIgnition delay-time study of fuel-rich CH 4 /air and CH 4 /additive/air mixtures over a wide temperature range at high pressure
25 th ICDERS August 2 7, 2015 Leeds, UK Ignition delay-time study of fuel-rich CH 4 /air and CH 4 /additive/air mixtures over a wide temperature range at high pressure Jürgen Herzler, Mustapha Fikri, Oliver
More informationUQ in Reacting Flows
UQ in Reacting Flows Planetary Entry Simulations High-Temperature Reactive Flow During descent in the atmosphere vehicles experience extreme heating loads The design of the thermal protection system (TPS)
More informationResults of turbulent flame speed for H 2 -rich and syngas fuel mixtures measured
Results of turbulent flame speed for H 2 -rich and syngas fuel mixtures measured Deliverable 1.1.4 SEVENTH FRAMEWORK PROGRAMME FP7-ENERGY-2008-TREN-1 ENERGY-2008-6-CLEAN COAL TECHNOLOGIES Project Acronym:
More informationLOW TEMPERATURE MODEL FOR PREMIXED METHANE FLAME COMBUSTION
ISTP-16, 2005, PRAGUE 16TH INTERNATIONAL SYMPOSIUM ON TRANSPORT PHENOMENA LOW TEMPERATURE MODEL FOR PREMIXED METHANE FLAME MBUSTION M. Forman, J.B.W.Kok,M. Jicha Department of Thermodynamics and Environmental
More informationTemperature time-history measurements in a shock tube using diode laser absorption of CO 2 near 2.7 µm
23 rd ICDERS July 24-29, 2011 Irvine, USA Temperature time-history measurements in a shock tube using diode laser absorption of CO 2 near 2.7 µm Wei Ren, Sijie Li, David F Davidson, and Ronald K Hanson
More informationA Comprehensive Modeling Study of Hydrogen Oxidation
A Comprehensive Modeling Study of Hydrogen Oxidation MARCUS Ó CONAIRE, 1 HENRY J. CURRAN, 2 JOHN M. SIMMIE, 1 WILLIAM J. PITZ, 3 CHARLES K. WESTBROOK 3 1 National University of Ireland, Galway, Ireland
More informationNumerical Study of Nitrogen Oxides (NOx) Formation in Homogenous System of Methane, Methanol and Methyl Formate at High Pressures
Numerical Study of Nitrogen Oxides (NOx) Formation in Homogenous System of Methane, Methanol and Methyl Formate at High Pressures J. M. Ngugi, P. N. Kioni, and J. K. Tanui Abstract The main aim of this
More informationFundamental Kinetics Database Utilizing Shock Tube Measurements
Fundamental Kinetics Database Utilizing Shock Tube Measurements Volume 3: Reaction Rate Measurements D. F. Davidson and R. K. Hanson Mechanical Engineering Department Stanford University, Stanford CA 94305
More informationUncertainty analysis of updated hydrogen and carbon monoxide oxidation mechanisms
Proceedings of the Combustion Institute 30 (2005) 1273 1281 Proceedings of the Combustion Institute www.elsevier.com/locate/proci Uncertainty analysis of updated hydrogen and carbon monoxide oxidation
More informationExperimental study of the combustion properties of methane/hydrogen mixtures Gersen, Sander
University of Groningen Experimental study of the combustion properties of methane/hydrogen mixtures Gersen, Sander IMPORTANT NOTE: You are advised to consult the publisher's version (publisher's PDF)
More informationModelling of transient stretched laminar flame speed of hydrogen-air mixtures using combustion kinetics
Loughborough University Institutional Repository Modelling of transient stretched laminar flame speed of hydrogen-air mixtures using combustion kinetics This item was submitted to Loughborough University's
More informationThe Seeding of Methane Oxidation
The Seeding of Methane Oxidation M. B. DAVIS and L. D. SCHMIDT* Department of Chemical Engineering and Materials Science, University of Minnesota, Minneapolis, MN 55455 USA Mixtures of light alkanes and
More informationarxiv: v1 [physics.chem-ph] 26 Apr 2011
Assessment of existing H 2 /O 2 chemical reaction mechanisms at reheat gas turbine conditions Torleif Weydahl a,, Madhavan Poyyapakkam b, Morten Seljeskog a, Nils Erland L. Haugen a arxiv:1104.4925v1 [physics.chem-ph]
More informationSkeletal Kinetic Mechanism of Methane Oxidation for High Pressures and Temperatures
7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Skeletal Kinetic Mechanism of Methane Oxidation for High Pressures and Temperatures Victor P. Zhukov and Alan F. Kong Institute of Space
More informationANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES
ANALYSIS OF THE PREDICTION ABILITY OF REACTION MECHANISMS FOR CFD MODELING OF THE COMBUSTION IN HIGH VELOCITY ENGINES V. Kopchenov*, S. Batura*, L. Bezgin*, N. Titova*, A. Starik* *CIAM, Russia Keywords:
More informationEXPERIMENTAL AND KINETIC
EXPERIMENTAL AND KINETIC MODELING STUDY OF THE EFFECT OF SO 2 ON FUEL OXIDATION IN AN O 2 /CO 2 ATMOSPHERE J. Giménez*, M. Martinez, A. Millera, R. Bilbao, M.U. Alzueta I3A - University of Zaragoza - Spain
More informationMethane Oxidation Reactions
Methane Oxidation Reactions CH 4 + 2 O -> CO 2 2 + 2 H 2 O Total Oxidation (Combustion) CH 4 + 0.5 O -> CO 2 + 2 H 2 CO + 0.5 O -> CO 2 2 H 2 + 0.5 O -> H 2 2 O CH 4 + H 2 O->CO + 3 H 2 Partial Oxidation
More informationEXPERIMENTAL AND NUMERICAL INVESTIGATION OF LAMINAR FLAME SPEEDS OF H 2 /CO/CO 2 /N 2 MIXTURES
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF LAMINAR FLAME SPEEDS OF H 2 /CO/CO 2 /N 2 MIXTURES A Dissertation Presented to The Academic Faculty by Jayaprakash Natarajan In Partial Fulfillment of the Requirements
More informationCOMBUSTION CHEMISTRY OF PROPANE: A CASE STUDY OF DETAILED REACTION MECHANISM OPTIMIZATION
Proceedings of the Combustion Institute, Volume 28, 2000/pp. 1663 1669 COMBUSTION CHEMISTRY OF PROPANE: A CASE STUDY OF DETAILED REACTION MECHANISM OPTIMIZATION ZHIWEI QIN, 1 VITALI V. LISSIANSKI, 1 HUIXING
More informationShock tube measurements of the tert-butanol + OH reaction rate and the tert-c 4 H 8 OH radical β-scission branching ratio using isotopic labeling
8 th U. S. National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013 Shock tube measurements of the tert-butanol
More informationAvailable online at Proceedings of the Combustion Institute 32 (2009)
Available online at www.sciencedirect.com Proceedings of the Combustion Institute 32 (29) 427 435 Proceedings of the Combustion Institute www.elsevier.com/locate/proci Oxidation of H 2 / 2 mixtures and
More informationHigh-Temperature Kinetics of AlCl 3 Decomposition in the Presence of Additives for Chemical Vapor Deposition
0013-4651/2002/149 5 /C261/7/$7.00 The Electrochemical Society, Inc. C261 High-Temperature Kinetics of AlCl 3 Decomposition in the Presence of Additives for Chemical Vapor Deposition Laurent Catoire a,z
More informationNumerical simulation study of turbulent combustion phenomena -INTEGRATE Advanced Study Group (ASG)
Numerical simulation study of turbulent combustion phenomena -INTEGRATE Advanced Study Group (ASG) Rixin Yu Division of fluid Mechanics Department of Energy Science LTH 1 Introduction Some combustion related
More informationAn Aromatics and cc 5 H 5-8 Model with Improved Transport for Flat Flames, Flow Reactors and Shock Tubes.
8 th US National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013 An Aromatics and cc 5 H 5-8 Model with Improved
More informationDynamics of Excited Hydroxyl Radicals in Hydrogen-Based Mixtures Behind Reflected Shock Waves
Dynamics of Excited Hydroxyl Radicals in Hydrogen-Based Mixtures Behind Reflected Shock Waves R. MÉVEL a, S. PICHON b, L. CATOIRE c, N. CHAUMEIX b, C.-E. PAILLARD b and J.E. SHEPHERD a Abstract a Graduate
More informationDevelopment of an Ethanol Combustion Mechanism Based on a Hierarchical Optimization Approach
Development of an Ethanol Combustion Mechanism Based on a Hierarchical Optimization Approach CARSTEN OLM, 1,2,3 TAMÁS VARGA, 1,2 ÉVA VALKÓ, 1,2 SANDRA HARTL, 3 CHRISTIAN HASSE, 3 TAMÁS TURÁNYI 1 1 Institute
More informationChemical Kinetic Optimization and Uncertainty Quantification
Chemical Kinetic Optimization and Uncertainty Quantification Tamás Turányi Institute of Chemistry, ELTE Eötvös Loránd University, Budapest, Hungary 8 March, 2018, Applied Mathematics Seminar, BME Greetings
More informationIGNITION DELAY TIME EXPERIMENTS FOR NATURAL GAS/HYDROGEN BLENDS AT ELEVATED PRESSURES
DRAFT Proceedings of ASME Turbo Expo 2013 GT2013 June 3-7, 2013, San Antonio, Texas, USA GT2013-95151 IGNITION DELAY TIME EXPERIMENTS FOR NATURAL GAS/HYDROGEN BLENDS AT ELEVATED PRESSURES Marissa L. Brower,
More informationComputational Study on the Recombination Reaction between Benzyl and Propargyl Radicals
The 7 th International Conference on Chemical Kinetics July 11, 2011 Computational Study on the Recombination Reaction between Benzyl and Propargyl Radicals Akira Matsugi and Akira Miyoshi Department of
More informationChemical Kinetics of Ethanol Oxidation. Tonawanda, NY 14150, USA. Princeton University Princeton, NJ 08544, USA
Chemical Kinetics of Ethanol xidation Juan Li 1, Andrei Kazakov 2, Frederick L. Dryer 2* 1 Praxair, Inc. Tonawanda, NY 1415, USA 2 Department of Mechanical and Aerospace Engineering Princeton University
More informationCOMBUSTION CHEMISTRY COMBUSTION AND FUELS
COMBUSTION CHEMISTRY CHEMICAL REACTION AND THE RATE OF REACTION General chemical reaction αa + βb = γc + δd A and B are substracts and C and are products, α, β, γ and δ are stoichiometric coefficients.
More informationA comparison of the Bader Deuflhard and the Cash Karp Runge Kutta integrators for the GRI-MECH 3.0 model based on the chemical kinetics code Kintecus
1368 A comparison of the Bader Deuflhard and the Cash Karp Runge Kutta integrators for the GRI-MECH 3.0 model based on the chemical inetics code Kintecus James C. Ianni Vast Technologies Development, Inc.,
More informationThermal NO Predictions in Glass Furnaces: A Subgrid Scale Validation Study
Feb 12 th 2004 Thermal NO Predictions in Glass Furnaces: A Subgrid Scale Validation Study Padmabhushana R. Desam & Prof. Philip J. Smith CRSIM, University of Utah Salt lake city, UT-84112 18 th Annual
More informationRECOMMENDED RATE CONSTANTS OF CHEMICAL REACTIONS IN AN H 2 -O 2 GAS MIXTURE WITH ELECTRONICALLY EXCITED SPECIES O 2 ( 1 ), O( 1 D), OH( 2 Σ) INVOLVED
RECOMMENDED RATE CONSTANTS OF CHEMICAL REACTIONS IN AN H 2 -O 2 GAS MIXTURE WITH ELECTRONICALLY EXCITED SPECIES O 2 ( 1 ), O( 1 D), OH( 2 Σ) INVOLVED L.B. Ibraguimova, G.D. Smekhov, O.P. Shatalov Institute
More informationThe evolution and cellular structure of a detonation subsequent to a head-on interaction with a shock wave
Combustion and Flame 151 (2007) 573 580 www.elsevier.com/locate/combustflame The evolution and cellular structure of a detonation subsequent to a head-on interaction with a shock wave Barbara B. Botros
More informationNon-Equilibrium Reaction Rates in Hydrogen Combustion
25 th ICDERS August 2 7, 25 Leeds, UK Non-Equilibrium Reaction Rates in Hydrogen Combustion Stephen J. Voelkel, Venkat Raman 2, Philip Varghese The University of Texas at Austin, Austin, TX 7872, USA 2
More informationPeculiarities of chemical transformations in the flames of mixtures of С1-С5 hydrocarbons with air and flammability concentration limits
Peculiarities of chemical transformations in the flames of mixtures of С1-С5 hydrocarbons with air and flammability concentration limits T.A. Bolshova, O.P. Korobeinichev, D.A. Knyazkov, A.G. Shmakov,
More informationDetailed chemistry models for butanols based on ab initio rate coefficients, and comparisons with experimental data
Detailed chemistry models for butanols based on ab initio rate coefficients, and comparisons with experimental data William H. Green, Michael Harper, Mary Schnoor, & Shamel Merchant CEFRC Annual Meeting
More informationHigh-pressure shock-tube study of the ignition of fuel-rich CH 4 /air and CH 4 /additive/air mixtures over a wide temperature range
High-pressure shock-tube study of the ignition of fuel-rich CH 4 /air and CH 4 /additive/air mixtures over a wide temperature range J. Herzler, M. Fikri, O. Welz, C. Schulz Institute for Combustion and
More informationAn Updated Reaction Model for the High-Temperature Pyrolysis and Oxidation of Acetaldehyde
Preprint, for published version see: R. Mevel, K. Chatelain, G. Blanquart, J. E. Shepherd "An updated reaction model for the high-temperature pyrolysis and oxidation of acetaldehyde" Fuel 217, 226-239,
More informationCalibration of the CO + OH CO 2 + H rate constant with direct and indirect information
Paper # 070RK-0246 Topic: Reaction Kinetics 8 th US National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013.
More informationSHOCK TUBE MEASUREMENTS OF OXYGENATED FUEL COMBUSTION USING LASER ABSORPTION SPECTROSCOPY
SHOCK TUBE MEASUREMENTS OF OXYGENATED FUEL COMBUSTION USING LASER ABSORPTION SPECTROSCOPY A DISSERTATION SUBMITTED TO THE DEPARTMENT OF MECHANICAL ENGINEERING AND THE COMMITTEE ON GRADUATE STUDIES OF STANFORD
More informationTHERMOCHEMICAL INSTABILITY OF HIGHLY DILUTED METHANE MILD COMBUSTION
THERMOCHEMICAL INSTABILITY OF HIGHLY DILUTED METHANE MILD COMBUSTION G. Bagheri*, E. Ranzi*, M. Lubrano Lavadera**, M. Pelucchi*, P. Sabia**, A. Parente***, M. de Joannon**, T. Faravelli* tiziano.faravelli@polimi.it
More informationThe influence of C ϕ is examined by performing calculations with the values C ϕ =1.2, 1.5, 2.0 and 3.0 for different chemistry mechanisms.
The Influence of Chemical Mechanisms on PDF Calculations of Nonpremixed Piloted Jet Flames Renfeng Cao and Stephen B. Pope Sibley School of Mechanical and Aerospace Engineering, Cornell University, Ithaca,
More informationKINETICS PATHS TO RADICAL-INDUCED IGNITION OF METHANE/AIR MIXTURES
Combust. Sci. and Tech., 177: 2275 2298, 2005 Copyright Q Taylor & Francis LLC ISSN: 0010-2202 print/1563-521x online DOI: 10.1080/00102200500241065 KINETICS PATHS TO RADICAL-INDUCED IGNITION OF METHANE/AIR
More informationUSE OF DETAILED KINETIC MODELS FOR MULTISCALE PROCESS SIMULATIONS OF SULFUR RECOVERY UNITS
USE OF DETAILED KINETIC MODELS FOR MULTISCALE PROCESS SIMULATIONS OF SULFUR RECOVERY UNITS F. Manenti*, D. Papasidero*, A. Cuoci*, A. Frassoldati*, T. Faravelli*, S. Pierucci*, E. Ranzi*, G. Buzzi-Ferraris*
More informationCH 4 /NO x Reduced Mechanisms Used for Modeling Premixed Combustion
Energy and Power Engineering, 2012, 4, 264-273 http://dx.doi.org/10.4236/epe.2012.44036 Published Online July 2012 (http://www.scirp.org/journal/epe) CH 4 /NO x Reduced Mechanisms Used for Modeling Premixed
More informationIn a high-temperature environment, such as the exit of the hot-air duct in the current counterflow
Appendix A: Thermocouple Radiation Correction In a high-temperature environment, such as the exit of the hot-air duct in the current counterflow arrangement, one major source of uncertainty in the measurement
More informationEFFECTS OF PRESSURE AND PREHEAT ON SUPER-ADIABATIC FLAME TEMPERATURES IN RICH PREMIXED METHANE/AIR FLAMES
Combust. Sci. and Tech., 180: 437 452, 2008 Copyright # Taylor & Francis Group, LLC ISSN: 0010-2202 print/1563-521x online DOI: 10.1080/00102200701741285 EFFECTS OF PRESSURE AND PREHEAT ON SUPER-ADIABATIC
More informationUTSR Fellowship Presentation Gas Turbine Industrial Fellowship Program 2006
UTSR Fellowship Presentation Gas Turbine Industrial Fellowship Program 2006 Predicting Lean Blowout Using the Damkohler Number Matthew J. Bloxham, Brigham Young University Ingersoll Rand Energy Systems
More informationFundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion. Andrey Starikovskiy Princeton University
Fundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion AFOSR MURI Review Meeting Andrey Starikovskiy Princeton University October 22, 2013 Report Documentation
More informationC. Saggese, N. E. Sanchez, A. Callejas, A. Millera, R. Bilbao, M. U. Alzueta, A. Frassoldati, A. Cuoci, T. Faravelli, E. Ranzi
Dipartimento di Chimica, Materiali e Ingegneria Chimica G. Natta Politecnico di Milano in collaboration with: A Kinetic Modeling Study of Polycyclic Aromatic Hydrocarbons (PAHs) and Soot Formation in Acetylene
More informationDevelopment of Constrained Equilibrium Codes and Their Applications in Nonequilibrium Thermodynamics
Partha S. Bishnu Djamel Hamiroune Mohamad Metghalchi e-mail: metghal@coe.neu.edu Mechanical, Industrial and Manufacturing Engineering Department, Northeastern University, Boston, MA 02115 Development of
More informationOxidation of C 3 and n-c 4 aldehydes at low temperatures
Oxidation of C 3 and n-c 4 aldehydes at low temperatures M. Pelucchi*, A. Frassoldati*, E. Ranzi*, T. Faravelli* matteo.pelucchi@polimi.it * CRECK-Department of Chemistry, Materials and Chemical Engineering
More informationChemical Kinetics: NOx Mechanisms
Mole Fraction Temperature (K) Chemical Kinetics: Nx Mechanisms Jerry Seitzman. 5.15.1.5 CH4 H HC x 1 Temperature Methane Flame.1..3 Distance (cm) 15 1 5 KineticsNx -1 Nx Formation Already pointed out that
More informationREDIM reduced modeling of quenching at a cold inert wall with detailed transport and different mechanisms
26 th ICDERS July 3 th August 4 th, 217 Boston, MA, USA REDIM reduced modeling of quenching at a cold inert wall with detailed transport and different mechanisms Christina Strassacker, Viatcheslav Bykov,
More informationDevelopment of an ethanol combustion mechanism based on a hierarchical optimization approach
Development of an ethanol combustion mechanism based on a hierarchical optimization approach C. Olm *,1,2,3, T. Varga 1,2, É. Valkó 1,2, S. Hartl 3, C. Hasse 3, T. Turányi 1 1 Laboratory for Chemical Kinetics,
More informationA Priori Model for the Effective Lewis Numbers in Premixed Turbulent Flames
Paper # 070LT-0267 Topic: Turbulent Flames 8 th US National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013.
More informationDetonations in mixtures containing nitrous oxide
Issw22 Detonations in mixtures containing nitrous oxide M. Kaneshige, E. Schultz, U.J. Pfahl, J.E. Shepherd, R. Akbar Graduate Aeronautical Laboratories, California Institute of Technology, Pasadena, CA
More informationROLE OF CHEMICAL KINETICS ON THE DETONATION PROPERTIES OF HYDROGEN / NATURAL GAS / AIR MIXTURES
ROLE OF CHEMICAL KINETICS ON THE DETONATION PROPERTIES OF HYDROGEN / NATURAL GAS / AIR MIXTURES Chaumeix 1 N., Pichon 1 S., Lafosse 1 F., Udari 1 N., Paillard 1,2 C.-E. 1 Laboratoire de Combustion et Systèmes
More informationLecture 2. Chemical Kinetics. Chemical Kinetics 6/26/11. One (elementary) step reaction
Lecture Chemical Kinetics 1 One (elementary) step reaction im i i M i is the number of species i, i are the stoichiometric coefficients i i Chemical Kinetics =0ifi is not a reactant =0ifi is not a product
More informationFundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion
Fundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion Walter R. Lempert, Igor V. Adamovich, J. William Rich, Jeffrey A. Sutton Department of Mechanical
More informationUNIVERSITY OF CALGARY. A Detailed Chemical Kinetics Mechanism for Biogas and Syngas Combustion. Hsu Chew Lee A THESIS
UNIVERSITY OF CALGARY A Detailed Chemical Kinetics Mechanism for Biogas and Syngas Combustion by Hsu Chew Lee A THESIS SUBMITTED TO THE FACULTY OF GRADUATE STUDIES IN PARTIAL FULFILLMENT OF THE REQUIREMENTS
More informationFUNDAMENTALS of Thermodynamics
SOLUTION MANUAL SI UNIT PROBLEMS CHAPTER 15 SONNTAG BORGNAKKE VAN WYLEN FUNDAMENTALS of Thermodynamics Sixth Edition CONTENT SUBSECTION PROB NO. Correspondence table Concept-Study Guide Problems 1-20 Equilibrium
More informationChemistry in society. Homework
hemistry in society Homework Equilibrium, Hess Law, Enthalpy 1 Multiple choice 10 marks 1) l 2 (g) + H 2 O(l) l - (aq) + lo - (aq) + 2H + (aq) The addition of which substance would move the above equilibrium
More information