Composite corrugated structures for morphing wing skin applications

By C. Thill, J. Etches, I. Bond, Kevin Potter, Paul M. Weaver. 2010

169 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Civil and Structural Engineering

View Paper: https://www.semanticscholar.org/paper/b7e6faee2ad5c8dd099525ce24ca654f9eb3d097

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Michael I. Friswell
2. E. S. Flores

In Civil and Structural Engineering

1. Michael I. Friswell
2. Alexander D. Shaw
3. E. S. Flores
4. I. Dayyani
5. J. Mottershead
6. H. H. Khodaparast

Citations in the corpus

• Equivalent models of corrugated panels (2012, methodology): “…then a suitable approach is the use of homogenisation techniques, in which the corrugated panel is replaced by an orthotropic plate with equivalent stiffness properties (Yokozeki et al., 2006; Thill et al., 2010a; Xia and Friswell, 2011). ll rights reserved. fax: +44 (0)1792 295157. riswell).”
• The mechanics of composite corrugated structures: A review with applications in morphing aircraft (2015, methodology): “This is due to the fact that wing structures must be stiff so as to withstand bending due to aerodynamic forces, and flexible so they can deform efficiently in flight due to morphing actuation [19].”