Topology Optimization of Compliant Adaptive Leading Edge with Geometrically Nonlinearity

Authors: Xin, Kou; Ge, Wenjie; Zhang, Yonghong

Source: Advanced Science Letters, Volume 4, Numbers 6-7, June/July 2011 , pp. 2306-2310(5)

Publisher: American Scientific Publishers

Buy & download fulltext article:

OR

Price: $113.00 plus tax (Refund Policy)

Abstract:

In flight, airfoil changes can significantly improve the aerodynamic performance and enhance the efficiency of aircraft. This paper introduces a systematic method to design compliant mechanisms to carry out airfoil required shape changes. Aiming at certain model unmanned aerial vehicle (UAV), the least square error between the deformed curve and the target curve is defined as the objective function, aerodynamic loads is defined as design condition. Based on variable density method, established the topology optimization model of adaptive wing leading edge which considered geometrically nonlinearity, and solved by using the method of moving asymptotes. Analyzing the results by ANSYS and experimental. The results show that the adaptive wing leading edge could make its shape change from 0 to 7.22 degrees. The experimental data show the feasibility of this approach.

Keywords: ADAPTIVE WING; COMPLIANT MECHANISM; GEOMETRICAL NONLINEARITY; TOPOLOGY OPTIMIZATION

Document Type: Research article

DOI: http://dx.doi.org/10.1166/asl.2011.1534

Publication date: 2011-06-01

More about this publication?
  • ADVANCED SCIENCE LETTERS is an international peer-reviewed journal with a very wide-ranging coverage, consolidates research activities in all areas of (1) Physical Sciences, (2) Biological Sciences, (3) Mathematical Sciences, (4) Engineering, (5) Computer and Information Sciences, and (6) Geosciences to publish original short communications, full research papers and timely brief (mini) reviews with authors photo and biography encompassing the basic and applied research and current developments in educational aspects of these scientific areas.
  • Editorial Board
  • Information for Authors
  • Subscribe to this Title
  • ingentaconnect is not responsible for the content or availability of external websites
Related content

Tools

Key

Free Content
Free content
New Content
New content
Open Access Content
Open access content
Subscribed Content
Subscribed content
Free Trial Content
Free trial content

Text size:

A | A | A | A
Share this item with others: These icons link to social bookmarking sites where readers can share and discover new web pages. print icon Print this page