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MATHEMATICAL MODELING
Numerical three-dimensional modeling of detonation wave rotation in a detonaton engine
Yu. G. Phyilippova, V. F. Nikitinab, E. V. Mikhalchenkoba, L. I. Stamovab a Lomonosov Moscow State University, Moscow, Russia
b Federal Science Center Scientific Research Institute for System Analysis of Russian Academy of Sciences,
Moscow, Russia
Abstract:
A three-dimensional numerical simulation of the combustion chamber of the engine with a rotating detonation wave (RDE) fed by hydrogen-air mixtures of different composition is carried out. A rotating detonation wave engine is a new type of engine capable of producing higher thrust than traditional engines based on the process of deflagration of a combustible mixture. The dynamic combustion process in RDE is more than 100 times faster than in the classical mode with slow deflagration combustion. This type of engine has a more efficient thermodynamic cycle. In numerical experiments, different compositions of the fuel mixture were tested, and different scenarios of the engine operation were obtained. In the computational domain, a regular grid of homogeneous cubic elements was used. Time-consuming parts of the numerical code were parallelized using the OpenMP technique. Calculations were carried out on the APK-5 with a maximum performance of 5.5 teraflops.
Keywords:
numerical simulation, detonation engine, chemical kinetics, deflagration, detonation, combustion chamber.
Citation:
Yu. G. Phyilippov, V. F. Nikitin, E. V. Mikhalchenko, L. I. Stamov, “Numerical three-dimensional modeling of detonation wave rotation in a detonaton engine”, Informatsionnye Tekhnologii i Vychslitel'nye Sistemy, 2019, no. 3, 87–98
Linking options:
https://www.mathnet.ru/eng/itvs356 https://www.mathnet.ru/eng/itvs/y2019/i3/p87
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Abstract page: | 71 | Full-text PDF : | 64 |
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