Journal
AIAA JOURNAL
Volume 61, Issue 5, Pages 2314-2318Publisher
AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.J062554
Keywords
Solid Rocket Motor; Heterogeneous Solid Propellant; Combustion Chambers; Courant Friedrichs Lewy Condition; Flame Temperature; Vortex Shedding Phenomena; Mass Flow Rate; Fluid Dynamics
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