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。
2
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。
3
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.