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Detonation engine fed by acetylene–oxygen mixture
Authors:NN Smirnov  VB Betelin  VF Nikitin  YuG Phylippov  Jaye Koo
Institution:1. Moscow M.V. Lomonosov State University, Moscow 119992, Russia;2. Scientific Research Institute for System Studies of Russian Academy of Sciences, Moscow 117218, Russia;3. School of Aerospace and Mechanical Engineering Korea Aerospace University, Goyang-city 411-791, Republic of Korea
Abstract:The advantages of a constant volume combustion cycle as compared to constant pressure combustion in terms of thermodynamic efficiency has focused the search for advanced propulsion on detonation engines. Detonation of acetylene mixed with oxygen in various proportions is studied using mathematical modeling. Simplified kinetics of acetylene burning includes 11 reactions with 9 components. Deflagration to detonation transition (DDT) is obtained in a cylindrical tube with a section of obstacles modeling a Shchelkin spiral; the DDT takes place in this section for a wide range of initial mixture compositions. A modified ka-omega turbulence model is used to simulate flame acceleration in the Shchelkin spiral section of the system. The results of numerical simulations were compared with experiments, which had been performed in the same size detonation chamber and turbulent spiral ring section, and with theoretical data on the Chapman–Jouguet detonation parameters.
Keywords:Detonation  Engine  Propulsion  Thermodynamic efficiency  Deflagration  Transition
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