Main weakness of hydrogen as a fuel is detonation fuel cycle that is more energetic favored in comparing with common fuel cycle [1]. In connection with this desire problem of hydrogen detonation turbine constructing is extreme real. Perspective results are projects of pulsing detonation turbine [1] and spin detonation motor [2,3]. Nowadays investigations in this field are given mainly by mathematical displaying methods. Essential part of examinations is developing and improving of numerical methods for mathematical simulation of deflagration initiation and change from deflagration to stable explosion in hydrogen-air gas mixes flows. From the kinetic point process of change to detonation can be doctored as transition from moderately deflagration to branching chain reaction in hydrogen-air join. These reactions place developed by N.N.Semenov [4]. The main aim of this paper is compering of forecast results with utilizing model of system of kinetic equating and one accompanying branching chain reaction.
Author(s) Details:
S. N. Martyushov,
Department
of Applied Mathematics and Physics, Moscow Aviation Institute – National
Research University, Volokolamskoye Shosse 4, Moscow 125995 308012, Russia.
Please see the link here: https://stm.bookpi.org/NACB-V7/article/view/11960
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