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Modelling of UAV's composite structures and prediction of safety factor

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper presents possibilities of composite materials modeling using SolidWorks enviroment on example of Unmanned Aerial Vehicle wing structure. Mechanical properties of composite materials used in UAV's and process of modeling such structures in SolidWorks are described. The research problem is CFD and strenght analysis of considered structure in SolidWorks Flow Simulation. Different displacement, stresses and safety factors values were obtained for analysed types of loads. The presented approach was used to develop aircraft wing for Air Challenge 2015 competition.
Słowa kluczowe
Rocznik
Strony
67--75
Opis fizyczny
Bibliogr. 8 poz., fig.
Twórcy
autor
  • Faculty of Mechanical Engineering, Bialystok University of Technology, Poland
  • Faculty of Mechanical Engineering, Bialystok University of Technology, Poland
  • Faculty of Mechanical Engineering, Bialystok University of Technology, Poland
Bibliografia
  • [1] Chung D.: Composite Materials – Science and Application. Springer 2010.
  • [2] Łukaszewicz A.: SolidWorks based CAx Education Directed for Industrial Practice. SolidWorks World 2010, Anaheim, USA, p. 23.
  • [3] Dankwort C., Weidlich R., Guenther B., Blaurock J. E.: Engineers’ CAx education-it’s not only CAD. Computer-Aided Design, Vol. 36, 2004, pp. 1439–1450.
  • [4] Planchard C., Planchard M.: SolidWorks 2011 Tutorial. Schroff Development Corporation, Mission KS, 2011.
  • [5] Lombard M.: SolidWorks 2010 Bible, Wiley Publishing, Indianapolis, USA, 2010.
  • [6] Grodzki W., Łukaszewicz A.: Design and manufacture of unmanned aerial vehicles (UAV) wing structure using composite materials. Materialwissenschaft und Werkstofftechnik, Vol. 46, No. 3, 2015, pp. 269–278.
  • [7] Karakas H., Koyunci E., Inalhan G.: ITU Tailless UAV Design. Journal of Intelligent and Robotic Systems, 2013, Vol. 69, p. 131.
  • [8] Grodzki W., Łukaszewicz A.: CAx tools in the design process of an unmanned flying device. Part 1 Aerodynamic analysis. Mechanik, Vol. 12, 2013, pp. 95–102.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-e90e67bd-5cf7-401d-ab45-bfaf7357d646
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