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Numerical modelling of detonation combustion of hydrogen-air mixture in a supersonic annular chamber Full article

Conference 3RD ALL-RUSSIAN SCIENTIFIC CONFERENCE THERMOPHYSICS AND PHYSICAL HYDRODYNAMICS WITH THE SCHOOL FOR YOUNG SCIENTISTS, TPH 2018 3RD ALL-RUSSIAN SCIENTIFIC CONFERENCE THERMOPHYSICS AND PHYSICAL HYDRODYNAMICS WITH THE SCHOOL FOR YOUNG SCIENTISTS
10-16 Sep 2018 , Ялта, Крым
Journal Journal of Physics: Conference Series
ISSN: 1742-6588
Output data Year: 2018, Volume: 1128, Article number : 012078, Pages count : 6 DOI: 10.1088/1742-6596/1128/1/012078
Authors Trotsyuk A V 1
Affiliations
1 Lavrentyev Institute of Hydrodynamics, Siberian Branch of the Russian Academy of Science

Funding (1)

1 Министерство науки и высшего образования Российской Федерации FWGG-2021-0003

Abstract: The flow structure for various detonation regimes is numerically studied in a new flow-type supersonic annular detonation combustor. In the combustor with a new design, detonation burning of the reacting mixture is organized by using a compression body, shaped as a continuous monofilar helix with a constant pitch angle. Numerical simulations are performed for a supersonic flow of a stoichiometric hydrogen-air mixture with Mach number M0=3 at the combustor entrance. A mathematical model of the reacting flow in the combustor is developed in a two-dimensional unsteady formulation. The flow dynamics at the beginning of combustor operation and the structure of the steady flow in the combustor are numerically studied. Simulations are performed for various helix angles and combustor sizes. A bifurcation of the steady flow structures with respect to the initial conditions of combustor operations is detected for some combinations of the geometric parameters of the combustor.
Cite: Trotsyuk A.V.
Numerical modelling of detonation combustion of hydrogen-air mixture in a supersonic annular chamber
Journal of Physics: Conference Series. 2018. V.1128. 012078 :1-6. DOI: 10.1088/1742-6596/1128/1/012078 Scopus РИНЦ OpenAlex
Identifiers:
Scopus: 2-s2.0-85058617950
Elibrary: 38637133
OpenAlex: W2904571640
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