Mechanical properties of corrugated composites for candidate materials of flexible wing structures

By T. Yokozeki, S. Takeda, T. Ogasawara, T. Ishikawa. 2006

316 citations recorded by the source corpus.

Subfields: Architecture, Civil and Structural Engineering, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/c9a51bc8f20bdb182717dc6ef2220341b29f8858

How researchers see this paper

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

In Architecture

1. E. Filipov
2. Glaucio H. Paulino
3. Tomohiro Tachi

In Civil and Structural Engineering

1. Michael I. Friswell
2. E. S. Flores
3. Jinsong Leng
4. Yanju Liu
5. Jian Sun
6. Qinghua Guan
7. E. Filipov
8. K. R. Olympio

In Mechanical Engineering

1. Jinsong Leng
2. Yanju Liu
3. Jian Sun
4. Qinghua Guan
5. E. Filipov
6. K. R. Olympio
7. Yuying Xia
8. Michael I. Friswell

Citations in the corpus

• Zero Poisson’s Ratio Cellular Honeycombs for Flex Skins Undergoing One-Dimensional Morphing (2010, background): “, 2005), corrugated skins with a face sheet (Yokozeki et al., 2006; Thill et al., 2007), and flexible matrix composite skins (Murray et al.”
• Flexible Skins for Morphing Aircraft Using Cellular Honeycomb Cores (2010, background): “Another approach considered by Yokozeki et al. (2006) and Thill et al. (2007) considered corrugated composites with a flexible face-sheet to create a smooth aerodynamic surface for flexible skins for 1D morphing applications.”
• The mechanics of composite corrugated structures: A review with applications in morphing aircraft (2015, background): “32. Queheillalt, D. T., Murty, Y., & Wadley, H. N. (2008). Mechanical properties of an extruded pyramidal lattice truss sandwich structure.”
• Equivalent models of corrugated panels (2012, methodology): “If the dimensions of the whole corrugated panel are much larger than the period of the corrugations, 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 ”
• Origami tubes assembled into stiff, yet reconfigurable structures and metamaterials (2015, background): “These phenomena make thin sheets practical for stiff and lightweight corrugated assemblies (5, 6); however, such systems tend to be static, i.”
• Composite corrugated structures for morphing wing skin applications (2010, background): “Yokozeki et al (2006) were among the first to suggest corrugated laminates made from carbon/epoxy composites for morphing wing skin applications.”
• Morphing aircraft based on smart materials and structures: A state-of-the-art review (2016, methodology): “One method is to fill the structure with flexible rubber (Yokozeki et al., 2006, 2014), and the other method is to cover it with a segmented skin similar to fish scales (Thill et al., 2010).”