Dye Visualization of the Flow Structure over a Yawed Nonslender Delta Wing

2009 ◽  
Vol 46 (5) ◽  
pp. 1818-1822 ◽  
Author(s):  
C. Canpolat ◽  
S. Yayla ◽  
B. Sahin ◽  
H. Akilli
Keyword(s):  
Flow Structure ◽  
Delta Wing ◽  
Dye Visualization

Critical states and flow structure on a 65-deg delta wing

1996 ◽  
Vol 33 (2) ◽  
pp. 347-352 ◽  
Author(s):  
Charles E. Jobe ◽  
Alexander H. Hsia ◽  
Jerry E. Jenkins ◽  
Gregory A. Addington
Keyword(s):  
Flow Structure ◽  
Delta Wing ◽  
Critical States

scholarly journals Effect of Thickness-to-Chord Ratio on Flow Structure of a Low Swept Delta Wing

AIAA Journal ◽  
2018 ◽  
Vol 56 (12) ◽  
pp. 4657-4668 ◽  
Author(s):  
Burak Gülsaçan ◽  
Gizem Şencan ◽  
Mehmet Metin Yavuz
Keyword(s):  
Flow Structure ◽  
Delta Wing

Effects of Trailing-Edge Attachment on the Flow Structure over a Generic Delta Wing

2017 ◽  
Vol 30 (5) ◽  
pp. 06017003
Author(s):  
C. Canpolat ◽  
S. Yayla ◽  
B. Sahin ◽  
H. Akilli
Keyword(s):  
Flow Structure ◽  
Delta Wing ◽  
Trailing Edge

Effect of Passive Bleeding on Flow Structure over a Nonslender Delta Wing

AIAA Journal ◽  
2017 ◽  
Vol 55 (8) ◽  
pp. 2555-2565 ◽  
Author(s):  
Alper Çelik ◽  
Cenk Çetin ◽  
Mehmet Metin Yavuz
Keyword(s):  
Flow Structure ◽  
Delta Wing

scholarly journals Flow Behavior in Side-View Plane of Pitching Delta Wing

2018 ◽  
Vol 180 ◽  
pp. 02080
Author(s):  
Mehmet Can Pektas ◽  
Mehmet Oguz Tasci ◽  
Ilyas Karasu ◽  
Besir Sahin ◽  
Huseyin Akilli
Keyword(s):  
Vortex Breakdown ◽  
Delta Wing ◽  
Flow Behavior ◽  
Side View ◽  
Visualization Technique ◽  
Sweep Angle ◽  
Pitching Motion ◽  
Reduced Frequency ◽  
Dye Visualization ◽  
Yaw Angle

In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcord according to the equation of α(t)=αm+α0sin(ωet). This study focused on understanding the effect of pitching and characterizing the interaction of vortex breakdown with oscillating leading edges under different yaw angles, β over a slender delta wing. The value of mean angle of attack, αm was taken as 25°. The yaw angle, β was varied with an interval of 4° over the range of 0°≤β≤ 16°. The delta wing was sinusoidally pitched within the range of period of time 5s≤Te≤60s and reduced frequency was set as K=0.16, 0.25, 0.49, 1.96 and lastly amplitude of pitching motion was arranged as α0=±5°.Formations and locations of vortex breakdown were investigated by using the dye visualization technique in side view plane.

Control of Flow Structure on Delta Wing with Steady Trailing-Edge Blow

AIAA Journal ◽  
2006 ◽  
Vol 44 (3) ◽  
pp. 493-501 ◽  
Author(s):  
M. M. Yavuz ◽  
D. Rockwell
Keyword(s):  
Flow Structure ◽  
Delta Wing ◽  
Trailing Edge ◽  
Control Of Flow

Flow Structure of Low-Aspect-Ratio Rotating Wings from Dye Visualization

AIAA Journal ◽  
2014 ◽  
Vol 52 (5) ◽  
pp. 1081-1086 ◽  
Author(s):  
Zakery R. Carr ◽  
Matthew J. Ringuette
Keyword(s):  
Aspect Ratio ◽  
Flow Structure ◽  
Low Aspect Ratio ◽  
Dye Visualization

Flow Structure on a Delta Wing of Low Sweep Angle

AIAA Journal ◽  
2004 ◽  
Vol 42 (3) ◽  
pp. 513-523 ◽  
Author(s):  
B. Yaniktepe ◽  
D. Rockwell
Keyword(s):  
Flow Structure ◽  
Delta Wing ◽  
Sweep Angle
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