Evolution of disturbances in the shock layer on a flat plate in the flow of a mixture of vibrationally excited gases

The results of the numerical and experimental investigations of the evolution of the disturbances in a hypersonic shock layer on a flat plate streamlined by a flow of the mixture of vibrationally excited gases are presented. The experimental study was conducted in the hot-shot high-enthalpy wind tun...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	Thermophysics and aeromechanics 2017-05, Vol.24 (3), p.421-430
Hauptverfasser:	Kirilovskiy, S. V., Poplavskaya, T. V., Tsyryulnikov, I. S., Maslov, A. A.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics CAD Carbon dioxide Carbon dioxide concentration Computational fluid dynamics Computer aided design Computer simulation Disturbances Evolution Fluid flow High enthalpy wind tunnels Hypersonic shock Mathematical models Modules Navier-Stokes equations Physics Physics and Astronomy Thermodynamics
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!