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- W2379494252 abstract "Based on the discrete particle model,the 3-D full-scale turbulent two-phase combustion flow in a LOX/Hydrogen rocket engine was numerically simulated by the PSIC algorithm.The Rosin-Rammler model was adopted to describe the distribution of the LOX spraying droplets whose mass averaged diameter was computed using the special spray model for the shear coaxial injector.In addition,the high pressure evaporation process was considered and the reaction rate was controlled by both the turbulent fluctuations method and the Arrhenius method.The spray distribution of LOX obtained by simulation is in agreement with that obtained from the hot-firing test of the engine,as well as other flow parameters.The models and the algorithm can also be used in simulation of combustion flow in other engines,which can provide foundational data for designing of the rocket engine." @default.
- W2379494252 created "2016-06-24" @default.
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- W2379494252 date "2011-01-01" @default.
- W2379494252 modified "2023-09-22" @default.
- W2379494252 title "Numerical Simulation of 3-D Full-scale Turbulent Two-phase Combustion Flow in LOX/Hydrogen Rocket Engine" @default.
- W2379494252 hasPublicationYear "2011" @default.
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