DocumentCode :
3292176
Title :
Investigation of Aerodynamic Characteristics of Blended-Wing-Body Aircraft Based on Cluster System
Author :
Zhang, Guo-qing ; Yang, Shu-xing ; Xue, Song-hai
Author_Institution :
Beijing Inst. of Tecnology. Beijing, Beijing, China
fYear :
2009
fDate :
6-7 June 2009
Firstpage :
253
Lastpage :
257
Abstract :
The aerodynamic characteristics of the BWB-UAV were simulated numerically based on the high performance computing cluster system. The effects on the aerodynamic characteristics of the whole aircraft made by the BWB were investigated. The longitudinal/lateral characteristics of BWB and the conventional tailless sweep wing had been compared. The results showed that BWB configuration had the better longitudinal aerodynamic characteristics. The causes of its excellent characteristics can be attributed to the new wing body lifting design, which can improve the flowing pattern of the surface. But its lateral stability was bad. Therefore, it would be an important criterion that trying to enhance the lateral stability in BWB-UAV design.
Keywords :
aerodynamics; aircraft; mechanical engineering computing; remotely operated vehicles; stability; vehicle dynamics; aerodynamic characteristics; blended-wing-body aircraft; high performance computing cluster system; lateral stability; longitudinal/lateral characteristics; surface flowing pattern; wing body lifting design; Aerodynamics; Aircraft; Computational fluid dynamics; Computational modeling; High performance computing; Mesh generation; Numerical simulation; Size control; Stability; Tail; BWB; Cluster System; mesh; stability; sweep wing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Web Mining and Web-based Application, 2009. WMWA '09. Second Pacific-Asia Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-0-7695-3646-0
Type :
conf
DOI :
10.1109/WMWA.2009.23
Filename :
5232513
Link To Document :
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