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Effect of ozone addition and ozonolysis reaction on the detonation properties of C2H4/O2/Ar mixtures
Institution:1. CAPT, SKLTCS, College of Engineering, Peking University, Beijing 100871, China;2. LCP, Institute of Applied Physics and Computational Mathematics, Beijing 100094, China;1. Department of Mechanical Engineering, National University of Singapore, 9 Engineering Drive 1, 117576 Singapore;2. Key laboratory for Thermal Science and Power Engineering of Ministry of Education, Department of Energy and Power Engineering, Tsinghua University, Beijing 100084, China;3. Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, New Jersey 08544, USA;4. Center for Combustion Energy, Tsinghua University, Beijing 100084, China;1. McGill University, Montreal, QC, Canada;2. Concordia University, Montreal, QC, Canada;3. University of Southampton, Southampton, United Kingdom;4. Department of Mechanical Engineering, Eindhoven University of Technology, Eindhoven, the Netherlands;5. Eindhoven Institute of Renewable Energy Systems, Eindhoven University of Technology, Eindhoven, the Netherlands;1. Department of Aerospace Engineering, Texas A&M University, College Station, TX 77840, USA;2. Department of Aerospace Engineering, University of Maryland, College Park, MD 20742, USA;1. Purdue University, West Lafayette, IN 47907, United States;2. California Institute of Technology, Pasadena, CA 91125, United States
Abstract:Ozone is one of the strongest oxidizers and can be used to enhance detonation. Detonation enhancement by ozone addition is usually attributed to the ozone decomposition reaction which produces reactive atomic oxygen and thereby accelerates the chain branching reaction. Recently, ozonolysis reaction has been found to be another mechanism to enhance combustion for unsaturated hydrocarbons at low temperatures. In this study, the effects of ozone addition and ozonolysis reaction on steady detonation structure and transient detonation initiation and propagation processes in C2H4/O2/O3/Ar mixtures are examined through simulations considering detailed chemistry. Specifically, the homogeneous ignition process, the ZND detonation structure, the transient direct detonation initiation, and pulsating instability of one-dimensional detonation propagation are investigated. It is found that the homogenous ignition process consists of two stages and the first stage is caused by ozonolysis reactions which consume O3 and produces CH2O as well as H and OH radicals. The ozonolysis reaction and ozone decomposition reaction can both reduce the induction length though they have little influence on the Chapman–Jouguet (CJ) detonation speed. The supercritical, critical and subcritical regimes for direct detonation initiation are identified by continuously decreasing the initiation energy or changing the amount of ozone addition. It is found that direct detonation initiation becomes easier at larger amount of ozone addition and/or larger reaction progress variable. This is interpreted based on the change of the induction length of the ZND detonation structure. Furthermore, it is demonstrated that the ozonolysis reaction can reduce pulsating instability and make the one-dimensional detonation propagation more stable. This is mainly due to the reduction in activation energy caused by ozone addition and/or ozonolysis reaction. This work shows that both ozone decomposition reaction and ozonolysis reaction can enhance detonation for unsaturated hydrocarbon fuels.
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