Helium bubble flow visualization of the spanwise separation on a NACA 0012 with simulated glaze ice

Author(s):  
M. KERHO ◽  
M. BRAGG ◽  
J. SHIN
1989 ◽  
Vol 26 (6) ◽  
pp. 499-502 ◽  
Author(s):  
Zhao Dong ◽  
Wang Zhongqi ◽  
Zhang Xiaodi ◽  
Qin Jialin ◽  
Lang Xianzhong

AIAA Journal ◽  
1965 ◽  
Vol 3 (6) ◽  
pp. 1203-1203 ◽  
Author(s):  
WILLIAM O. CRIMINALE ◽  
R. W. NOWELL

AIAA Journal ◽  
1969 ◽  
Vol 7 (8) ◽  
pp. 1635-1637 ◽  
Author(s):  
FREDERICK W. ROOS ◽  
WILLIAM W. WILLMARTH

1979 ◽  
Vol 101 (3) ◽  
pp. 376-380 ◽  
Author(s):  
K. W. McAlister ◽  
L. W. Carr

A two-dimensional experiment was conducted in a water tunnel using hydrogen bubble flow visualizations for the purpose of exposing, independently, the behavior of the viscous and inviscid domains during unsteady airfoil stall. By imposing a large amplitude pitch oscillation about the static-stall angle of a modified NACA 0012 airfoil, an unsteady environment was created that not only altered considerably the progression of flow reversal along the airfoil surface from what was observed in steady flow, but also caused a unique succession of vortical developments to appear that is unparalleled in steady flow.


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