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Towards Direct Numerical Simulations of Reactivity-Controlled Compression Ignition Engine Using n-Octanol/Ethanol Fuel Blends

Flow Turbulence and Combustion, vol. 115, pp. 275–301

Abstract

Abstract The results of a two-dimensional direct numerical simulation of a lean n-octanol-ethanol fuel blend under Reactivity Controlled Compression Ignition (RCCI) conditions are presented in this paper. Stratified temperature and high reactivity fuel fields of Gaussian, bi-modal, and log-normal distributions are studied for uncorrelated and correlated scenarios. The pimple loop is made to run twice to achieve compression heating. A chemical mechanism with 171 species and 734 reactions was developed to capture autoignition characteristics and flame propagation reasonably well. Diagnosing techniques published in the literature are used to determine whether the flame fronts are spontaneously propagating or not. As reported previously for other fuel blends under RCCI conditions, both deflagration and spontaneous ignition flame fronts are observed to co-exist. Gaussian, bi-modal, and log-normal fields respectively move towards a spontaneously igniting mode. Correlating temperature and high reactivity fuel fields not only makes combustion more spontaneously igniting but also more premixed. The analysis reveals the sensitivity of the DNS results with respect to the initial conditions which accordingly should be chosen with care.

Authors 4

  1. Universität der Bundeswehr München

    Affiliation as printed

    Department of Aerospace Engineering, Institute of Applied Mathematics and Scientific Computing, University of the Bundeswehr Munich, Werner-Heisenberg-Weg 39, 85577, Neubiberg, Germany

  2. RWTH Aachen University

    Affiliation as printed

    Faculty of Mechanical Engineering, Institute for Combustion Technology, RWTH Aachen University, Templergraben 64, 52056, Aachen, Germany

  3. RWTH Aachen University

    Affiliation as printed

    Faculty of Mechanical Engineering, Institute for Combustion Technology, RWTH Aachen University, Templergraben 64, 52056, Aachen, Germany

  4. Markus Klein corresponding

    Universität der Bundeswehr München

    Affiliation as printed

    Department of Aerospace Engineering, Institute of Applied Mathematics and Scientific Computing, University of the Bundeswehr Munich, Werner-Heisenberg-Weg 39, 85577, Neubiberg, Germany

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References 33