Abstract:In a solid rocket motor (SRM), when the propellant combusts, the aluminum is oxidized into alumina (Al 2 O 3 ) which, under the right flow conditions, tends to agglomerate into molten droplets, impinge on the chamber walls, and then flow along the nozzle wall. Such agglomerates can cause erosive damage. The focus of the current research is to characterize the agglomerate flow within the nozzle section by studying the breakup process of a liquid film that flows along the wall of a straight channel while a high-… Show more
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