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
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;
Conference_Titel :
Business, Engineering and Industrial Applications (ICBEIA), 2011 International Conference on
Conference_Location :
Kuala Lumpur
Print_ISBN :
978-1-4577-1279-1
DOI :
10.1109/ICBEIA.2011.5994261
