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Sibley School of Mechanical and Aerospace Engineering

New article: A Chemical Mechanism for Low to High Temperature Oxidation of Methylcyclohexane as a Component of Transportation Fuel Surrogates

Article:  Narayanaswamy, K; Pitsch, H; and Pepiot, P; (2015)  “A Chemical Mechanism for Low to High Temperature Oxidation of Methylcyclohexane as a Component of Transportation Fuel Surrogates”, Combustion and Flame, 162 (4):1193-1213

DOI

Abstract:  Surrogate fuels consisting of a mixture of well-studied hydrocarbons are often used to model real fuels in typical combustion studies. A major challenge, however, is the capability to design compact and reliable kinetic models that capture all the specificities of the simpler, but still multi-component surrogates. This task is further complicated by the diverse nature of the hydrocarbons commonly considered as potential surrogate components, since they typically result in large detailed reaction schemes. Towards addressing this challenge, the present work proposes a single, compact, and reliable chemical mechanism, that can accurately describe the oxidation of a wide range of fuels, which are important components of surrogate fuels. A well-characterized mechanism appropriate for the oxidation of smaller hydrocarbon species (Blanquart et al., 2009), as well as several substituted aromatic species and n-dodecane (Narayanaswamy et al., 2010, 2014), well suited as a base to model surrogates, has now been extended to describe the oxidation of methylcyclohexane, a representative of the cyclic alkane class, which is often used in jet fuel surrogates. To ensure compactness of the kinetic scheme, a short mechanism for the low to high temperature oxidation of methylcyclohexane is extracted from the detailed scheme of Fitz et al.
(2007) and integrated in a systematic way into the previous model. Rate coefficient changes based on recent recommendations from literature, and an additional concerted elimination pathway important at moderate to low temperatures are introduced to the resulting chemical mechanism, which improve the model predictions. Extensive validation of the revised kinetic model is performed using a wide range of experimental conditions and data sets. Published by Elsevier Inc. on behalf of The Combustion Institute.

Funding Acknowledgement:  AFOSR; NASA; SERDP [WP-2151]; German Research Foundation (DFG) within the Collaborative Research Centre – Model-Based Control of Homogenized Low-Temperature Combustion at RWTH Aachen University, Germany [SFB 686]; Bielefeld University, Germany; U.S. Department of Energy, Office of Science, Office of Basic Energy Sciences [DE-FG02 – 90ER14128]

Funding Text:  The first and the third author gratefully acknowledge funding by the AFOSR and NASA, in addition to support by SERDP under Grant WP-2151 with Dr. Robin Nissan as the program manager. The third author also acknowledges support from the German Research Foundation (DFG) within the Collaborative Research Centre SFB 686 – Model-Based Control of Homogenized Low-Temperature Combustion at RWTH Aachen University, Germany, and Bielefeld University, Germany. This material is also based upon work supported by the U.S. Department of Energy, Office of Science, Office of Basic Energy Sciences, under Award Number DE-FG02 – 90ER14128. The authors would like to thank Dr. Fei Qi, Zhandong Wang, and their co-workers for sharing their raw measurements for species profiles in flames and permitting to use their experimental data. The authors are also grateful to Prof. Elizabeth Fisher for her assistance in testing the mechanism files in chemkin format. The authors would also like to acknowledge the insightful comments of the reviewers, which helped improve the quality of this article significantly.

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