Experimental and numerical study of the aerodynamic drag crisis phenomenon of a symmetrical thick teardrop airfoil with rounded trailing edge

A symmetrical thick teardrop airfoil with rounded trailing edge was investigated in this article. The airfoil is typical for frames, masts and other structural elements. Aerodynamic forces were measured in Reynolds number range from 1·104 to 10·104 and angle of attack range from −10° to +10°. Critic...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Akimov, M. A., Budovskiy, A. D., Obuhovskiy, A. D., Polivanov, P. A.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamic drag Aerodynamic forces Aerodynamics Angle of attack Critical angle Fluid flow Masts Reynolds number Structural members Trailing edges Zero angle of attack
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!