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- W2358052129 abstract "A three-dimensional(3-D) numerical simulation of aerodynamic throat formed by secondary flow from round injectors,which was applied to solid propellant rocket motors,was performed in this paper.The typical 3-D flow structure and mass flow character of round injectors were reviewed.The influence of different injector area ratios,injector numbers,injection angles,injector types and major nozzle parameter were studied.The results show that the mass control performance of aerodynamic throat can be obviously improved by increasing injector numbers,applying reverse injection or convergence injector type at the same injector area ratio." @default.
- W2358052129 created "2016-06-24" @default.
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- W2358052129 date "2011-01-01" @default.
- W2358052129 modified "2023-09-24" @default.
- W2358052129 title "Steady numerical study of aerodynamic throat formed by round injectors" @default.
- W2358052129 hasPublicationYear "2011" @default.
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