2016
DOI: 10.1177/1045389x16629569
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Morphing aircraft based on smart materials and structures: A state-of-the-art review

Abstract: A traditional aircraft is optimized for only one or two flight conditions, not for the entire flight envelope. In contrast, the wings of a bird can be reshaped to provide optimal performance at all flight conditions. Any change in an aircraft’s configuration, in particular the wings, affects the aerodynamic performance, and optimal configurations can be obtained for each flight condition. Morphing technologies offer aerodynamic benefits for an aircraft over a wide range of flight conditions. The advantages of … Show more

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Cited by 267 publications
(146 citation statements)
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“…For example, the auxetic properties are known to increase the shear and indentation resistance, and provide strain amplification . The shape re‐configuration capabilities by folding have great potentials in shape morphing for high performance aircrafts and vehicles . Studies on the nonlinear stiffness properties of origami can lay down the foundation for building relatively light, stiff, yet reconfigurable materials for adaptive civil infrastructures .…”
Section: Folding Induced Mechanical Propertiesmentioning
confidence: 99%
“…For example, the auxetic properties are known to increase the shear and indentation resistance, and provide strain amplification . The shape re‐configuration capabilities by folding have great potentials in shape morphing for high performance aircrafts and vehicles . Studies on the nonlinear stiffness properties of origami can lay down the foundation for building relatively light, stiff, yet reconfigurable materials for adaptive civil infrastructures .…”
Section: Folding Induced Mechanical Propertiesmentioning
confidence: 99%
“…The increased drag is due in part to the discontinuities in the aerodynamic surfaces caused by traditional discrete, mechanism-based (e.g., trailing edge flaps) control surfaces. To improve upon this situation, there has been growing interest in the use of adaptive or morphing structures to create smooth and continuous changes in wing shape ( Barbarino et al (2011), Sun et al (2016)), in a manner which removes the discontinuities of traditional approaches and allows for more complex, three-dimensional changes in shape.…”
Section: Removing Discontinuities From Aerodynamic Surfacesmentioning
confidence: 99%
“…Other authors observe that composites present a good fatigue performance. 24,25 Barbarino et al 19 state that "SMA fatigue behaviour shall be verified by appropriate experimental campaigns," and Sun et al 26 remark, ominously, that "SMA, SMP, and EAP have poor anti-fatigue ability,"…”
Section: Introductionmentioning
confidence: 99%