DocumentCode
2899110
Title
Airframe design for modularity of the BWB Baseline II-E2 UAV
Author
Katon, Matzaini ; Kuntjoro, Wahyu
Author_Institution
Fac. of Mech. Eng., Univ. Teknol. MARA, Shah Alam, Malaysia
fYear
2011
fDate
5-7 June 2011
Firstpage
73
Lastpage
77
Abstract
This paper discusses the airframe design of UiTM´s Blended Wing Body (BWB) Baseline II-E2 Unmanned Aerial Vehicle (UAV). The design concept is based on the modularity. The BWB airframe was modeled by using Computer Aided Design (CAD) software. Static analysis on the BWB airframe was conducted by using the Finite Element (FE) analysis. Airframe design, stress and displacement contours are presented.
Keywords
CAD; aerospace components; aerospace engineering; aerospace robotics; blending; finite element analysis; BWB baseline II-E2 UAV; airframe design; blended wing body baseline II-E2 unmanned aerial vehicle; computer aided design software; displacement contours; finite element analysis; static analysis; stress contours; Aluminum; Design automation; Force; Skin; BWB; CAD; UAV; airframe design; fastener design; finite element analysis; modularity;
fLanguage
English
Publisher
ieee
Conference_Titel
Business, Engineering and Industrial Applications (ICBEIA), 2011 International Conference on
Conference_Location
Kuala Lumpur
Print_ISBN
978-1-4577-1279-1
Type
conf
DOI
10.1109/ICBEIA.2011.5994261
Filename
5994261
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