Three dimensional investigation of the shock train structure in a convergent–divergent nozzle

Three-dimensional computational fluid dynamics analyses have been employed to study the compressible and turbulent flow of the shock train in a convergent-divergent nozzle. The primary goal is to determine the behavior, location, and number of shocks. In this context, full multi-grid initialization,...

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Veröffentlicht in:	Acta astronautica 2014-12, Vol.105 (1), p.117-127
Hauptverfasser:	Mousavi, Seyed Mahmood, Roohi, Ehsan
Format:	Artikel
Sprache:	eng
Schlagworte:	Compressibility Computational fluid dynamics Computer programs Convergent-divergent nozzles Heat generation Three dimensional Trains Turbulent flow
Online-Zugang:	Volltext
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