Title
Methane/propane oxidation at high pressures: Experimental and detailed chemical kinetic modeling
Abbreviated Journal Title
Proc. Combust. Inst.
Keywords
ignition; methane; propane; shock tube; chemical kinetics; fuel blends; high pressure; REFLECTED SHOCK-WAVES; OXYGEN-ARGON MIXTURES; GAS-TURBINE COMBUSTOR; IGNITION DELAY TIMES; NATURAL-GAS; TEMPERATURE; CH3+O-2; MECHANISM; ETHANE; FUELS; Thermodynamics; Energy & Fuels; Engineering, Chemical; Engineering, ; Mechanical
Abstract
Shock tube experiments and chemical kinetic modeling were performed to further understand the ignition and oxidation kinetics of various methane-propane fuel blends at gas turbine pressures. Ignition delay times were obtained behind reflected shock waves for fuel mixtures consisting of CH4/C3H8 in ratios ranging from 90/10% to 60/40%. Equivalence ratios varied from lean (phi = 0.5), through stoichiometric to rich (phi = 3.0) at test pressures from 5.3 to 31.4 atm. These pressures and mixtures, in conjunction with test temperatures as low as 1042 K, cover a critical range of conditions relevant to practical turbines where few, if any, CH4/C3H8 prior data existed. A methane/propane oxidation mechanism was prepared to simulate the experimental results. It was found that the reactions involving CH3O, CH3O2, and CH3 + O-2/HO2 chemistry were very important in reproducing the correct kinetic behavior. (C) 2006 Published by Elsevier Inc. on behalf of The Combustion Institute.
Journal Title
Proceedings of the Combustion Institute
Volume
31
Publication Date
1-1-2007
Document Type
Article
Language
English
First Page
447
Last Page
454
WOS Identifier
ISSN
1540-7489
Recommended Citation
"Methane/propane oxidation at high pressures: Experimental and detailed chemical kinetic modeling" (2007). Faculty Bibliography 2000s. 7523.
https://stars.library.ucf.edu/facultybib2000/7523
Comments
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