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Finite Element Analysis of a Thin Walled Composite Wing by Including Warping Effects

[+] Author Affiliations
Ozge Ozdemir Ozgumus, Seher Durmaz, Metin Orhan Kaya

Istanbul Technical University, Istanbul, Turkey

Paper No. IMECE2010-40418, pp. 209-214; 6 pages
doi:10.1115/IMECE2010-40418
From:
  • ASME 2010 International Mechanical Engineering Congress and Exposition
  • Volume 13: Sound, Vibration and Design
  • Vancouver, British Columbia, Canada, November 12–18, 2010
  • Conference Sponsors: ASME
  • ISBN: 978-0-7918-4450-2
  • Copyright © 2010 by ASME

abstract

The purpose of the present paper is to develop a finite element code to model a thin-walled composite beam. The beam is modeled as a thin-walled composite beam with a single-cell, rectangular cross-section featuring both CAS and CUS lay-up configurations. Analytical and finite element formulations of the flapwise bending, chordwise bending and torsional displacements of the beam are derived. Effect of the ply orientation on the natural frequencies is investigated and it is noticed that the obtained results are in good agreement with the ones in open literature.

Copyright © 2010 by ASME

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