Pressure Gradient and Nonadiabatic Surface Effects on Boundary Layer Transition

The influence of the streamwise pressure gradient and a nonadiabatic surface on boundary layer transition was experimentally investigated at the Cryogenic Ludwieg-Tube Göttingen, Germany. Boundary layer transition was detected nonintrusively by means of the temperature-sensitive paint technique. The...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	AIAA journal 2016-11, Vol.54 (11), p.3465-3480
Hauptverfasser:	Costantini, Marco, Hein, Stefan, Henne, Ulrich, Klein, Christian, Koch, Stefan, Schojda, Lukas, Ondrus, Vladimir, Schröder, Wolfgang
Format:	Artikel
Sprache:	eng
Schlagworte:	Boundary layer stability Boundary layer transition Compressibility Computational fluid dynamics Flow stability Fluid flow High Reynolds number Mach number Model testing Parallel flow Pressure gradients Reynolds number Temperature gradients Temperature ratio Temperature-sensitive paints Wall temperature Wind tunnel models Wind tunnels
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!