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Numerical analysis of the influence of two-phase flow mass and heat transfer on n-heptane autoignition
Authors:Zakaria Bouali  Cecile Pera  Julien Reveillon
Affiliation:1. Department of Mechanical Engineering, Khalifa University of Science, Technology and Research, Abu Dhabi 127788, United Arab Emirates;2. Clean Combustion Research Center (CCRC), King Abdullah University of Science and Technology (KAUST), Thuwal 23955-6900, Saudi Arabia;3. Combustion Research Facility, Sandia National Laboratories, Livermore, CA 94551, United States;4. Aerospace and Mechanical Engineering Department, University of Notre Dame, Notre Dame, IN, United States;5. Mechanical and Aerospace Engineering Department, Sapienza University, Rome 00184, Italy;1. Center for Combustion Energy, Tsinghua University, Beijing 100084, China;2. Department of Mechanical Engineering, Oakland University, Rochester, MI 48309, USA;3. School of Aerospace Engineering, Tsinghua University, Beijing 100084, China;4. State Key Laboratory of Automotive Safety and Energy, Tsinghua University, Beijing 100084, China;5. Aramco Services Company, Aramco Research Center-Detroit, Novi, MI 48377, USA;6. Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA
Abstract:This paper investigates the influence of liquid fuel presence on the autoignition of n-heptane/air mixtures over a wide range of conditions encountered in internal combustion engines. To this end, evaporating droplet physics and skeletal chemistry mechanisms are simultaneously solved considering a homogeneous constant-pressure reactor. A skeletal mechanism is introduced to account for specific kinetics behavior in the Negative Temperature Coefficient (NTC) region. The impact of mass and heat source terms during evaporation is emphasized by comparing a two-phase flow scenario with a purely gaseous case. The competition between fuel vapor availability and the evaporation-induced gas temperature decrease is specific to two-phase flow autoignition. On the one hand, droplet evaporation delay restricts the gaseous local fuel/air equivalence ratio and consequently the kinetics runaway. On the other hand, temperature reduction due to evaporation may either reduce or enhance chemical reactivity, depending on the local thermodynamic conditions lying either inside or outside the NTC region. By simultaneously accounting for evaporation source terms and skeletal chemistry, we can reproduce the already experimentally observed transformation of the NTC region into a Zero Temperature Coefficient (ZTC) region depending on thermodynamic conditions and droplet size. The ZTC phenomenon appears when combustion heat-release starts before complete droplet evaporation. Since the ZTC behavior can be captured using the point source approach, in which droplets are considered only as zero-dimensional source terms of mass and energy, the present results pave the way for future exploration of NTC chemistry in sprays with a direct numerical simulation of discrete particles considering detailed chemistry and turbulent flows.
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