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- W195584530 abstract "Abstract : The objective of this research was to improve understanding of the mechanisms by which flow, mixing and combustion processes are coupled to acoustic fields in liquid-propellant rocket motors. Particular attention was focused on analyses of amplification mechanisms coupled with finite-rate chemical reactions by use of numerical and analytical methods. Special attention was focused on LOX/GH2 systems and suggested a possible explanation of threshold phenomena found in liquid-propellant rockets. Reduced chemistry was developed for describing LOX combustion in GH2. and approaches towards explaining droplet burning-time minima in the transcritical regime were completed. The results can be helpful in improving knowledge of combustion mechanisms and combustion instability in liquid-propellant rocket motors at high pressures." @default.
- W195584530 created "2016-06-24" @default.
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- W195584530 date "1999-12-29" @default.
- W195584530 modified "2023-09-22" @default.
- W195584530 title "Fundamentals of Acoustic Instabilities in Liquid Propellant Rockets Under Transcritical Conditions." @default.
- W195584530 doi "https://doi.org/10.21236/ada372407" @default.
- W195584530 hasPublicationYear "1999" @default.
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