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Apologies for the quick and dirty question, but I was wondering if a computational fluid dynamics analysis of the flow inside a rocket's combustion chamber and nozzle area would be regarded as an analysis of the chamber's/nozzle's internal ballistics. Looking up internal ballistics on wiki, it only gives a single line regarding rockets: "For rocket propelled projectiles, internal ballistics covers the period during which a rocket motor is providing thrust."
Any help would be appreciated
Any help would be appreciated