And the time lag of evaporation and decomposition has been utilized to analyze the combustion instability.
用蒸发和分解的时滞来分析燃烧不稳定性。
In this paper, one-dimensional two-phase constant lag flow in combustion chamber of solid propellant rocket motors is described.
本文论述了固体火箭发动机燃烧室一维两相常滞后流动。
Small amounts of fuel are introduced into the combustion chamber prior to the main injection event, reducing lag time and promoting more continuous and complete combustion.
少量的燃油被引入燃烧室的主要注射液事件之前，减少滞后时间，促进更多的连续和完整的燃烧。
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