Experimental investigation of flow past simple model bodies in hypersonic wind tunnels at similar values of the Mach and Reynolds numbers but at different physical flow velocities

The pressure distributions over the surfaces of simple model bodies, such as hemisphere, wedge, and cone, and the bow shock stand-off distances from these bodies are investigated in hypersonic wind tunnels with similar-in-value Mach and Reynolds numbers but considerably different flow velocities ( u...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Fluid dynamics 2015, Vol.50 (1), p.109-117
Hauptverfasser:	Alferov, V. I., Bushmin, A. S., Egorov, I. V.
Format:	Artikel
Sprache:	eng
Schlagworte:	Classical and Continuum Physics Classical Mechanics Engineering Fluid Dynamics Fluid- and Aerodynamics Physics Physics and Astronomy
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!