Flow structure in the wake of a space-launcher model with propulsive-jet simulation
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DOI: 10.1007/s12567-020-00306-8
Abstract: The flow around a space launcher is dominated by flow separation at the junction between the main body and engine and strongly influenced by the propulsive jet. The flow field is highly unsteady with strong… read more here.
Keywords: space; launcher; jet; model ... See more keywords