Acoustic pressure oscillation effects on mean burning rates of plateau propellants
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DOI: 10.1016/j.combustflame.2020.11.018
Abstract: Abstract Combustion instabilities constitute a well pronounced problem in all large rocket motors due to the inherent acoustic pressure oscillations established based on the port geometries. Suppression of the combustion instabilities in the solid rocket… read more here.
Keywords: burning rates; acoustic pressure; burning rate; mean burning ... See more keywords