Effect of Thrust-Vectoring Jets on Delta Wing Aerodynamics

2007 ◽  
Vol 44 (6) ◽  
pp. 1877-1888 ◽  
Author(s):  
Zhi-Jin Wang ◽  
Ping Jiang ◽  
Ismet Gursul
Keyword(s):  
Delta Wing ◽  
Thrust Vectoring ◽  
Wing Aerodynamics

Wind-Tunnel Interference Effects on Delta Wing Aerodynamics Computational Fluid Dynamics Investigation

2005 ◽  
Vol 42 (1) ◽  
pp. 189-198 ◽  
Author(s):  
M. R. Allan ◽  
K. J. Badcock ◽  
G. N. Barakos ◽  
B. E. Richards
Keyword(s):  
Fluid Dynamics ◽  
Computational Fluid Dynamics ◽  
Wind Tunnel ◽  
Delta Wing ◽  
Interference Effects ◽  
Wing Aerodynamics

Multifaceted Influence of Fuselage Geometry on Delta-Wing Aerodynamics

2003 ◽  
Vol 40 (1) ◽  
pp. 204-206 ◽  
Author(s):  
Lars E. Ericsson
Keyword(s):  
Delta Wing ◽  
Wing Aerodynamics

scholarly journals Development of Delta Wing Aerodynamics Research in Universiti Teknologi Malaysia Low Speed Wind Tunnel

2014 ◽  
Vol 6 ◽  
pp. 434892 ◽  
Author(s):  
Shabudin Mat ◽  
I. S. Ishak ◽  
Tholudin Mat Lazim ◽  
Shuhaimi Mansor ◽  
Mazuriah Said ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Delta Wing ◽  
Low Speed ◽  
Low Speed Wind Tunnel ◽  
Wing Aerodynamics

Recent developments in delta wing aerodynamics

2004 ◽  
Vol 108 (1087) ◽  
pp. 437-452 ◽  
Author(s):  
I. Gursul
Keyword(s):  
Shear Layer ◽  
Vortex Breakdown ◽  
Delta Wing ◽  
Layer Structure ◽  
Vortical Flow ◽  
Time Lags ◽  
Delta Wings ◽  
Vortex Interactions ◽  
Recent Developments ◽  
Wing Aerodynamics

Abstract Recent developments in delta wing aerodynamics are reviewed. For slender delta wings, recent investigations shed more light on the unsteady aspects of shear-layer structure, vortex core, breakdown and its instabilities. For nonslender delta wings, substantial differences in the structure of vortical flow and breakdown may exist. Vortex interactions are generic to both slender and nonslender wings. Various unsteady flow phenomena may cause buffeting of wings and fins, however, vortex breakdown, vortex shedding, and shear layer reattachment are the most dominant sources. Dynamic response of vortex breakdown over delta wings in unsteady flows can be characterised by large time lags and hysteresis, whose physical mechanisms need further studies. Unusual flow–structure interactions for nonslender wings in the form of self-excited roll oscillations have been observed. Recent experiments showed that substantial lift enhancement is possible on a flexible delta wing.

Double-delta-wing aerodynamics for pitching motions with and without sideslip

1995 ◽  
Vol 32 (6) ◽  
pp. 1303-1311 ◽  
Author(s):  
Deborah S. Grismer ◽  
Robert C. Nelson
Keyword(s):  
Delta Wing ◽  
Double Delta Wing ◽  
Wing Aerodynamics
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