Trailing-edge jet control of leading-edge vortices of a delta wing

AIAA Journal ◽  
1996 ◽  
Vol 34 (7) ◽  
pp. 1447-1457 ◽  
Author(s):  
Chiang Shih ◽  
Zhong Ding
Keyword(s):  
Delta Wing ◽  
Leading Edge ◽  
Trailing Edge ◽  
Jet Control ◽  
Leading Edge Vortices

Errata: Trailing-Edge Jet Control of Leading-Edge Vortices of a Delta Wing

AIAA Journal ◽  
1996 ◽  
Vol 34 (12) ◽  
pp. 2642-2644 ◽  
Author(s):  
Chiang Shih ◽  
Zhong Ding
Keyword(s):  
Delta Wing ◽  
Leading Edge ◽  
Trailing Edge ◽  
Jet Control ◽  
Leading Edge Vortices

The effect of a 70 deg swept canard on the leading-edge vortices of a 70 deg swept delta wing during dynamic pitching

1997 ◽  
Author(s):  
Shigeo Hayashibara ◽  
Roy Myose ◽  
L. Miller ◽  
Shigeo Hayashibara ◽  
Roy Myose ◽  
...  
Keyword(s):  
Delta Wing ◽  
Leading Edge ◽  
Leading Edge Vortices

0526 PIV Measurement on Leading Edge Vortices of a Delta Wing

2014 ◽  
Vol 2014 (0) ◽  
pp. _0526-1_-_0526-2_
Author(s):  
Tadateru ISHIDE ◽  
Hiroyuki ISHIKAWA ◽  
Kazuya NAGANUMA ◽  
Sinsuke SEIJI ◽  
Sumika FUJIMOTO ◽  
...  
Keyword(s):  
Delta Wing ◽  
Leading Edge ◽  
Piv Measurement ◽  
Leading Edge Vortices

Characterization of a Three-Dimensional Leading-Edge Separation Bubble on Swept, Low Aspect-Ratio Propeller Blades

2017 ◽  
Author(s):  
Ye-Bonne Koyama Maldonado ◽  
Gregory Delattre ◽  
Cedric Illoul ◽  
Clement Dejeu ◽  
Laurent Jacquin
Keyword(s):  
Delta Wing ◽  
Separation Bubble ◽  
Three Dimensional ◽  
Leading Edge ◽  
Time Resolved ◽  
Leading Edge Vortex ◽  
Wall Structures ◽  
Edge Vortex ◽  
Propeller Blades ◽  
Leading Edge Vortices

Leading-edge vortex flows are often present on propeller blades at take-off, however, their characteristics and aerodynamic impact are still not fully understood. An experimental investigation using Time Resolved Particle Image Velocimetry (TR-PIV) has been performed on a model blade in order to classify this flow with respect to both delta wing leading-edge vortices and the low Reynolds number studies regarding leading-edge vortices on rotating blades. A numerical calculation of the experimental setup has been performed in order to assess usual numerical methods for propeller performance prediction against TR-PIV results. Similar characteristics were found with non slender delta wing vortices at low incidence, which hints that the leading-edge vortex flow may generate vortex lift. The influence of rotation on the characteristics of the leading-edge vortex is compared to that of the pressure gradient caused by the circulation distribution. A discussion on the quality of the PIV reconstruction for close-wall structures is provided.

Quantitative visualization of the leading-edge vortices on a delta wing by using pressure-sensitive paint

2001 ◽  
Vol 4 (2) ◽  
pp. 139-150 ◽  
Author(s):  
Y. Egami ◽  
Y. Iijima ◽  
Y. Amao ◽  
K. Asai ◽  
A. Fuji ◽  
...  
Keyword(s):  
Delta Wing ◽  
Leading Edge ◽  
Pressure Sensitive Paint ◽  
Pressure Sensitive ◽  
Quantitative Visualization ◽  
Leading Edge Vortices
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