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Concept Design of Composite Aircraft Wing

[+] Author Affiliations
J. S. Rao

Altair Engineering India Pvt Ltd., Bangalore, KA, India

S. Kiran

Autolive India Pvt Ltd., Bangalore, KA, India

Paper No. IMECE2010-37206, pp. 51-59; 9 pages
doi:10.1115/IMECE2010-37206
From:
  • ASME 2010 International Mechanical Engineering Congress and Exposition
  • Volume 1: Advances in Aerospace Technology
  • Vancouver, British Columbia, Canada, November 12–18, 2010
  • Conference Sponsors: ASME
  • ISBN: 978-0-7918-4425-0
  • Copyright © 2010 by ASME

abstract

This paper is concerned with an optimal concept design of aircraft wing from an airfoil. The airfoil itself is generated from CFD studies but there is no baseline of the wing structure. Topology optimization is recently applied for weight reduction given an operating baseline structure; here it is demonstrated that this optimization can be used to derive the concept of the wing structure directly. The optimized concept design is realized in to CAD and then a composite free-size optimization is performed to determine material distribution and ply drop regions etc. Finally a composite size and shape optimization is done and the ribs thus realized are presented.

Copyright © 2010 by ASME

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