Supercritical airfoil drag reduction by passive shock wave/boundary layer control in the Mach number range .75 to .90

1985 ◽  
Author(s):  
H. NAGAMATSU ◽  
R. FICARRA
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Mach Number ◽  
Drag Reduction ◽  
Boundary Layer Control ◽  
Number Range ◽  
Supercritical Airfoil ◽  
Wave Boundary Layer ◽  
Wave Boundary ◽  
Layer Control

Passive shock-wave/boundary-layer control on a wall-mounted model

AIAA Journal ◽  
1987 ◽  
Vol 25 (2) ◽  
pp. 275-278 ◽  
Author(s):  
S. Raghunathan ◽  
D. G. Mabey
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Boundary Layer Control ◽  
Wave Boundary Layer ◽  
Wave Boundary ◽  
Layer Control

scholarly journals Passive shock wave/boundary layer control of wing at transonic speeds

2017 ◽  
Vol 7 (6) ◽  
pp. 325-330 ◽  
Author(s):  
Ling Zhou ◽  
Dehua Chen ◽  
Yang Tao ◽  
Guangyuan Liu ◽  
Shuheng Song ◽  
...  
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Boundary Layer Control ◽  
Wave Boundary Layer ◽  
Wave Boundary ◽  
Layer Control
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