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With the aim to develop more efficient aircraft configurations, the Blended-Wing-Body (BWB) unmanned aerial vehicles have grown attention in recent years. Compare to conventional aircraft configurations, the BWB structure has several advantages in aerody- namics and fuel efficiency. Topology optimization (TO) is also a relatively new structure optimization approach which has applied successfully in automotive industry for a consid- erable time. In this paper, topology optimization method will be applied on a special BWB structure UAV called BITU on both 2D and 3D models in ABAQUS. The optimization goal is to minimize compliance energy under specified loading and boundary conditions which will be computed in modeling and simulation section. Finally, optimized result compared to initial design will demonstrate TO is a rational and efficient design tool for structure optimization, especially in Aircraft industry.
Resume in LuaLatex Resume in LuaLatex using json sources. Work in progress on HTML page based on the same json sources.
Sjabloon Jinkampvoorbereiding volgens richtlijnen Scouts en Gidsen Vlaanderen
Thesis template for UASLP
Presentation for Final Project - Theory of Computation
A thesis/dissertation template for the students of Sharif University of Technology.
A new algorithm can speed up searching anything as a generalization of B/R-Trees
An English version of the master thesis template at Charles University in Prague, Faculty of Mathematics and Physics. Originates from http://mj.ucw.cz/vyuka/bc, exports to PDF/A. Valid as of 2017/04/19
Modelo de TCC da Engenharia da UFJF
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