Interaction of steady gasodynamic discontinuities and waves on supersonic gas jet flows from rocket engines

New analytical model of jet flow with Mach shock reflection is proposed. Gas flowfield is separated to several regions, and model problem of interaction between gasodynamic discontinuities and Prandtl-Meyer waves is solved in the each of them. Simple approximate analytical soutions are provided for...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Alekseeva, Mariya M., Matveev, Stanislav A., Savelova, Karina E., Chernyshov, Mikhail V.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Discontinuity Gas jets Jet flow Mathematical models Rocket engines Shock waves
Online-Zugang:	Volltext
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